NACA Digital Library - UK Mirror

    372 records

  1. Simon Ostrach; An analysis of laminar free-convection flow and heat transfer about a flat plate paralled to the direction of the generating body force; naca-report-1111; 1953

  2. Vernon A. Slabey, Paul H. Wise, Louis C. Gibbons; Hydrocarbon and nonhydrocarbon derivatives of cyclopropane; naca-report-1112; 1953

  3. H. S. Ribner, M. Tucker; Spectrum of turbulence in a contracting stream; naca-report-1113; 1953

  4. Benjamin Pinkel, Irvin M. Karp; A thermodynamic study of the turbine-propeller engine; naca-report-1114; 1953

  5. John D. Stanitz; Design of two-dimensional channels with prescribed velocity distributions along the channel walls; naca-report-1115; 1953

  6. John D. Stanitz, Leonard J. Sheldrake; Application of a channel design method to high-solidity cascades and tests of an impulse cascade with 90 degrees of turning; naca-report-1116; 1953

  7. Herbert F. Hardrath, Lachlan Ohman; A study of elastic and plastic stress concentration factors due to notches and fillets in flat plates; naca-report-1117; 1953

  8. E. R. Eckert, John N. B. Livingood; Method for calculation of laminar heat transfer in air flow around cylinders of arbitrary cross section (including large temperature differences and transpiration cooling); naca-report-1118; 1953

  9. Max A. Heaslet, John R. Spreiter; Reciprocity relations in aerodynamics; naca-report-1119; 1953

  10. Dwight G. Moore, Mary A. Mason, William N. Harrison; Relative importance of various sources of defect-producing hydrogen introduced into steel during application of vitreous coatings; naca-report-1120; 1953

  11. Satish Dhawan; Direct measurements of skin friction; naca-report-1121; 1953

  12. Sheldon Paul Rideout, Paul A. Beck; Survey of portions of the chromium-cobalt-nickel-molybdenum quaternary system at 1,200 degrees c; naca-report-1122; 1953

  13. A. J. Eggers, Clarence A. Syvertson, Samuel Kraus; A study of inviscid flow about airfoils at high supersonic speeds; naca-report-1123; 1953

  14. Franklin K. Moore; Displacement effect of a three-dimensional boundary layer; naca-report-1124; 1953

  15. Harold Gold, Edward W. Otto, Victor L. Ransom; Dynamics of mechanical feedback-type hydraulic servomotors under inertia loads; naca-report-1125; 1953

  16. Julian D. Maynard, Seymour Steinberg; The effect of blade-section thickness ratio on the aerodynamic characteristics of related full-scale propellers at Mach numbers up to 0.65; naca-report-1126; 1953

  17. Robert E. English, Richard H. Cavicchi; One-dimensional analysis of choked-flow turbines; naca-report-1127; 1953

  18. Herbert C. Nelson, Julian H. Berman; Calculations on the forces and moments for an oscillating wing-aileron combination in two-dimensional potential flow at sonic speed; naca-report-1128; 1953

  19. Bernard Budiansky, Edwin T. Kruszewski; Transverse vibrations of hollow thin-walled cylindrical beams; naca-report-1129; 1953

  20. John D. Bird, Lewis R. Fisher, Sadie M. Hubbard; Some effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yaw; naca-report-1130; 1953

  21. Manuel Stein, Edward Anderson, John Hedgepeth; Deflection and stress analysis of thin solid wings of arbitrary plan form with particular reference to delta wings; naca-report-1131; 1953

  22. Franklin K. Moore; Laminar boundary layer on cone in supersonic flow at large angle of attack; naca-report-1132; 1953

  23. I. Irving Pinkel, G. Merritt Preson, Gerard J. Pesman; Mechanism of start and development of aircraft crash fires; naca-report-1133; 1953

  24. Donald R. Bellman, Jack C. Humphrey, Theodore Male; Photographic investigation of combustion in a two-dimensional transparent rocket engine; naca-report-1134; 1953

  25. Ames Research Staff; Equations, tables, and charts for compressible flow; naca-report-1135; 1953

  26. Ralph W. Stone, Jr.; Estimation of the maximum angle of sideslip for determination of vertical-tail loads in rolling maneuvers; naca-report-1136; 1953

  27. Almer D. Crim, John P. Reeder, James B. Whitten; Initial results of instrument-flying trials conducted in a single-rotor helicopter; naca-report-1137; 1953

  28. Henry A. Pearson; Study of inadvertent speed increases in transport operation; naca-report-1138; 1953

  29. Kenneth A. Foss, Franklin W. Diederich; Charts and approximate formulas for the estimation of aeroelastic effects of the lateral control of swept and unswept wings; naca-report-1139; 1953

  30. Franklin W. Diederich, Kenneth A. Foss; Charts and approximate formulas for the estimation of aeroelastic effects on the loading of swept and unswept wings; naca-report-1140; 1953

  31. George B. Brajnikoff; Method and graphs for the evaluation of air-induction systems; naca-report-1141; 1953

  32. Mahinder S. Uberoi, Stanley Corrsin; Diffusion of heat from a line source in isotropic turbulence; naca-report-1142; 1953

  33. John C. Martin; A vector study of linearized supersonic flow applications to nonplanar problems; naca-report-1143; 1953

  34. John M. Riebe, Rodger L. Naeseth; Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes; naca-report-1144; 1953

  35. John A. Zalovick, Lindsay J. Lina, James P. Trant, Jr.; A method of calibrating airspeed installations on airplanes at transonic and supersonic speeds by the use of accelerometer and attitude-angle measurements; naca-report-1145; 1953

  36. Jones F. Cahill, William J. Underwood, Robert J. Nuber, Gail A. Cheesman; Aerodynamic forces and loadings on symmetrical circular-arc airfoils with plain leading-edge and plain trailing-edge flaps; naca-report-1146; 1953

  37. Frank M. Hamaker, Stanford E. Neice, Thomas J. Wong; The similarity law for hypersonic flow and requirements for dynamic similarity of related bodies in free flight; naca-report-1147; 1953

  38. M. M. Frocht, R. Guernsey, Jr.; A special investigation to develop a general method for three-dimensional photoelastic stress analysis; naca-report-1148; 1953

  39. Carl Kaplan; On transonic flow past a wave-shaped wall; naca-report-1149; 1953

  40. Harry L. Runyan, Charles E. Watkins; Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow; naca-report-1150; 1953

  41. Robert O. Schade, James L. Hassell, Jr.; The effects on dynamic lateral stability and control of large artificial variations in the rotary stability derivatives; naca-report-1151; 1953

  42. Emanuel Schnitzer; Theory and procedure for determining loads and motions in chine-immersed hydrodynamic impacts of prismatic bodies; naca-report-1152; 1953

  43. John R. Spreiter; On the application of transonic similarity rules to wings of finite span; naca-report-1153; 1953

  44. Benjamin Milwitzky, Francis E. Cook; Analysis of landing-gear behavior; naca-report-1154; 1953

  45. Clarence W. Matthews; A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory; naca-report-1155; 1953

  46. Fred S. Elwell; Experiments to determine neighborhood reactions to light airplanes with and without external noise reduction; naca-report-1156; 1953

  47. Geoge B. Dubois, Fred W. Ocvirk; Analytical derivation and experimental evaluation of short-bearing approximation for full journal bearing; naca-report-1157; 1953

  48. B. J. Saelman, H. W. Vick; Weight bar charts; naca-rm-53b19; Jun 1953

  49. Edmund E. Callaghan, John S. Serafini; Analytical investigation of icing limit for diamond-shaped airfoil in transonic and supersonic flow; naca-tn-2861; Jan 1953

  50. Thomas F. Gelder, James P. Lewis, Stanley L. Koutz; Icing protection for a turbojet transport airplane : heating requirements methods of protection, and performance penalties; naca-tn-2866; Jan 1953

  51. Y. S. Tang, J. M. Duncan, H. E. Schweyer; Heat and momentum transfer between a spherical particle and air streams; naca-tn-2867; Mar 1953

  52. Alfred Ritter, Yung-Huai Kuo; Reflection of a weak shock wave from a boundary layer along a flat plate I : interaction of weak shock waves with laminar and turbulent boundary layers analyzed by momentum-integral method; naca-tn-2868; Jan 1953

  53. Yung-Huai Kuo; Reflection of weak shock wave from a boundary layer along a flat plate II : interaction of oblique shock wave with a laminar boundary layer analyzed by differential-equation method; naca-tn-2869; Jan 1953

  54. S. E. Slaymaker, Robin B. Gray; Power-off flare-up tests of a model helicopter rotor in vertical autorotation; naca-tn-2870; Jan 1953

  55. Thomas W. Wilder, III, William A. Brooks, Jr., Eldon E. Mathauser; The effect of initial curvature on the strength of an inelastic column; naca-tn-2872; Jan 1953

  56. Paul Seide; The effect of longitudinal stiffeners located on one side of a plate on the compressive buckling stress of the plate-stiffener combination; naca-tn-2873; Jan 1953

  57. J. Mayers, Robert W. Fralich, Eric Reissner; Behavior in pure bending of a long monocoque beam of circular-arc cross section; naca-tn-2875; Jan 1953

  58. Derrill B. Chambliss, George M. Boyd, Jr.; The planing characteristics of two V-shaped prismatic surfaces having angles of dead rise of 20 degrees and 40 degrees; naca-tn-2876; Jan 1953

  59. Melvin Sadoff; On the use of a damped sine-wave elevator motion for computing the design maneuvering horizontal-tail load; naca-tn-2877; Jan 1953

  60. Maurice Tucker; Combined effect of damping screens and streams convergence on turbulence; naca-tn-2878; Jan 1953

  61. Bert A. Coss, D. R. Daykin, Leonard Jaffe, Elmer M. Sharp; A digital automatic multiple pressure recorder; naca-tn-2880; Jan 1953

  62. William Solomon; Aerodynamic characteristics of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller; naca-tn-2881; Jan 1953

  63. Albert J. Evans; The zero-lift drag of a slender body of revolution (NACA RM-10 research model) as determined from tests in several wind tunnels and in flight at supersonic speeds; naca-tn-2944; Apr 1953

  64. R. D. Johnson, F. R. Shober, A. D. Schwope; The creep of single crystals of aluminum; naca-tn-2945; May 1953

  65. M. John Pilny; A small Pirani gage for measurements of nonsteady low pressures; naca-tn-2946; Jun 1953

  66. Walter F. Lindsey, Joseph Burlock; A variable-frequency light synchronized with a high-speed motion-picture camera to provide very short exposure times; naca-tn-2949; May 1953

  67. Eugene S. Love, Carl E. Grigsby; A new shadowgraph technique for the observation of conical flow phenomena in supersonic flow and preliminary results obtained for a triangular wing; naca-tn-2950; May 1953

  68. Harold N. Murrow, Chester B. Payne; Flight investigation of the effect of transient wing response on wing strains of a four-engine bomber airplane in rough air; naca-tn-2951; Jun 1953

  69. Rinaldo J. Brun, Helen M. Gallagher, Dorothea E. Vogt; Impingement of water droplets on NACA 65(1)-208 and 65(1)-212 airfoils at 4 degrees angle of attack; naca-tn-2952; May 1953

  70. John R. Meyer, Gaetano Falabella, Jr.; An investigation of the experimental aerodynamic loading on a model helicopter rotor blade; naca-tn-2953; May 1953

  71. Percy J. Bobbitt, Frank S. Malvestuto, Jr.; Estimation of forces and moments due to rolling for several slender-tail configurations at supersonic speeds; naca-tn-2955; Jul 1953

  72. Charles Libove; Creep-buckling analysis of rectangular-section columns; naca-tn-2956; Jun 1953

  73. Vernon L. Rogallo, John L. McCloud, III; Surveys of the flow fields at the propeller planes of six 40 degree sweptback wing-fuselage-nacelle combinations; naca-tn-2957; Jun 1953

  74. Charles E. Frank, Angus U. Blackham; Reaction processes leading to spontaneous ignition of hydrocarbons; naca-tn-2958; Jun 1053

  75. Doris Cohen, Morris D. Friedman; Theoretical investigation of the supersonic lift and drag of thin, sweptback wings with increased sweep near the root; naca-tn-2959; Jun 1953

  76. Forrest E. Gowen, Edward W. Perkins; Drag of circular cylinders for a wide range of Reynolds numbers and Mach numbers; naca-tn-2960; Jun 1953

  77. Chung-Hua Wu; Subsonic flow of air through a single-stage and a seven-stage compressor; naca-tn-2961; Jun 1953

  78. Vernon H. Gray, Uwe H. Von Glahn; Effect of ice and frost formations on drag of NACA 65(1)-212 airfoil for various modes of thermal ice protection; naca-tn-2962; Jun 1953

  79. Norris F. Dow, William A. Hickman, B. Walter Rosen; Effect of variation in rivet strength on the average stress at maximum load for aluminum-alloy, flat, Z-stiffened compression panels that fail by local buckling; naca-tn-2963; Jun 1953

  80. Thomas L. Coleman, Paul W. J. Schumacher; An analysis of normal-acceleration and airspeed data from a four-engine type of transport; naca-tn-2965; Aug 1953

  81. Jean Gilman, Jr.; Propeller-performance charts for transport airplanes; naca-tn-2966; Jul 1953

  82. Albert E. Von Doenhoff, George W. Jones, Jr.; An analysis of the power-off landing maneuver in terms of the capabilities of the pilot and the aerodynamic characteristics of the airplane; naca-tn-2967; Aug 1953

  83. Dwight G. Moore, Mary A. Mason; Investigation of gases evolved during firing of vitreous coatings on steel; naca-tn-2865; Jan 1953

  84. Leslie S. G. Kovasznay; Development of turbulence-measuring equipment; naca-tn-2839; Jan 1953

  85. Robert D. Ingebo; Study of pressure effects on vaporization rate of drops in gas streams; naca-tn-2850; Jan 1953

  86. Harry Press, Bernard Mazelsky; A study of the application of power-spectral methods of generalized harmonic analysis to gust loads on airplanes; naca-tn-2853; Jan 1953

  87. Morton Cooper, John R. Sevier, Jr.; Estimated power reduction by water injection in a nonreturn supersonic wind tunnel; naca-tn-2856; Jan 1953

  88. Abramovitz, Marvin; Theoretical investigation of the performance of proportional navigation guidance systems : effect of missile configuration on the speed of response; naca-rm-a52j22; January 19, 1953

  89. Conrad, E William Essig, Robert H Finger, Harold B; Effect of rotor- and stator-blade modifications on surge performance of an 11-stage axial-flow compressor II : redesigned compressor for XJ-40-WE-6 engine; naca-rm-e52i10; May 25, 1953

  90. John J. Rebeske, Jr., James F. Dugan, Jr.; Matched performance characteristics of a 16-stage axial-flow compressor and a 3-stage turbine; naca-rm-e52h18; Apr 1953

  91. Joseph T. Hamrick, Walter M. Osborn, William L. Beede; Design and test of mixed-flow impellers III : design and experimental results for impeller model MFI-2A and comparison with impeller model MFI-1A; naca-rm-e52l22a; Mar 1953

  92. Neice, Stanford E Wong, Thomas J; An experimental investigation of the applicability of the hypersonic similarity law to bodies of revolution; naca-rm-a52k07; January 27, 1953

  93. Mead, Merrill H; Experimental investigation of the aerodynamic characteristics of an air-to-air missile employing cruciform wings and tail of rectangular plan form at Mach numbers of 1.4 and 1.9; naca-rm-a52k14; February 16, 1953

  94. Boyd, John W Pfyl, Frank A; Experimental investigation of aerodynamically balanced trailing-edge control surfaces on an aspect ratio 2 triangular wing at subsonic and supersonic speeds; naca-rm-a52l04; February 13, 1953

  95. Tobak, Murray; Damping in pitch of low-aspect-ratio wings at subsonic and supersonic speeds; naca-rm-a52l04a; April 08, 1953

  96. Koenig, David G; Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect ratio 3 triangular wing and an all-movable horizontal tail : longitudinal and lateral characteristics; naca-rm-a52l15; April 13, 1953

  97. Heitmeyer, John C; Effect of vertical position of the wing on the aerodynamic characteristics of three wing-body combinations; naca-rm-a52l15a; February 18, 1953

  98. Swift, John T Scherrer, Richard Stroud, John F; Preliminary investigation of a variable-area auxiliary air-intake system at Mach numbers from 0 to 1.3; naca-rm-a53a13; February 25, 1953

  99. Hall, Charles F; Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds; naca-rm-a53a30; April 14, 1953

  100. Syvertson, Clarence A Gloria, Hermilo R; An experimental investigation of the zero-lift-drag characteristics of symmetrical blunt-trailing-edge airfoils at Mach numbers from 2.7 to 5.0; naca-rm-a53b02; April 29, 1953

  101. Holdaway, George H; Comparison of the aerodynamic characteristics at transonic speeds of a plane wing and a cambered and twisted wing, both having 45 degrees of sweepback and an aspect ratio of 6; naca-rm-a53b16; May 05, 1953

  102. Allen, Edwin C; Experimental investigation of the effects of plan-form taper on the aerodynamic characteristics of symmetrical unswept wings of varying aspect ratio; naca-rm-a53c19; May 29, 1953

  103. Smith, Donald W Reed, Verlin D; Subsonic static longitudinal stability and control characteristics of a wing-body combination having a pointed wing of aspect ratio 2 with constant-percent-chord trailing-edge elevons; naca-rm-a53c20; May 22, 1953

  104. James, Carlton S Carros, Robert J; Experimental investigation of the zero-lift drag of a fin-stabilized body of fineness ratio 10 at Mach numbers between 0.6 and 10; naca-rm-a53d02; June 11, 1953

  105. Spahr, J Richard Dickey, Robert R; Wind-tunnel investigation of the vortex wake and downwash field behind triangular wings and wing-body combinations at supersonic speeds; naca-rm-a53d10; June 25, 1953

  106. Reese, David E , Jr; An experimental investigation at subsonic and supersonic speeds of the torsional damping characteristics of a constant-chord control surface of an aspect ratio 2 triangular wing; naca-rm-a53d27; July 02, 1953

  107. Frazer, Alson C Anderson, Warren E; Performance of a normal-shock scoop inlet with boundary-layer control; naca-rm-a53d29; June 29, 1953

  108. Brajnikoff, George B Stroud, John F; Experimental investigation of the effect of entrance width-to-height ratio on the performance of an auxiliary scoop-type inlet at Mach numbers from 0 to 1.3; naca-rm-a53e28; July 30, 1953

  109. Jorgensen, Leland H; Correlation by the hypersonic similarity rule of the pressure distributions and wave drags for minimum-drag nose shapes at zero angle of attack; naca-rm-a53f12; August 31, 1953

  110. Holdaway, George H; Comparison of theoretical and experimental zero-lift drag-rise characteristics of wing-body-tail combinations near the speed of sound; naca-rm-a53h17; October 16, 1953

  111. Edwards, Sherman Hikido, Katsumi; A method for estimating the rolling moments caused by wing-tail interference for missiles at supersonic speeds; naca-rm-a53h18; November 12, 1953

  112. Gowen, Forrest E Perkins, Edward W; A study of the effects of body shape on the vortex wakes of inclined bodies at a Mach number of 2; naca-rm-a53i17; December 1953

  113. Lazzeroni, Frank A; Investigation of a missile airframe with control surfaces consisting of projecting quadrants of the nose cone; naca-rm-a53l21; March 15, 1953

  114. Dangle, E E Cervenka, A J Bahr, D W; Effects of fuel temperature and fuel distribution on the combustion efficiency of a 16-inch ram-jet engine at a simulated Mach number of 2.9; naca-rm-e52j14; January 08, 1953

  115. Allen, J L Beke, Andrew; Force and pressure recovery characteristics at supersonic speeds of a conical spike inlet with bypasses discharging in an axial direction; naca-rm-e52k14; January 30, 1953

  116. Hearth, Donald P Gorton, Gerald C; Investigation at supersonic speeds of an inlet employing conical flow separation from a probe ahead of a blunt body; naca-rm-e52k18; January 19, 1953

  117. Disher, John H Kohl, Robert C Jones, Merle L; Free-flight performance of a rocket-boosted, air-launched 16-inch-diameter ram-jet engine at Mach numbers up to 2.20; naca-rm-e52l02; February 03, 1953

  118. Medeiros, Arthur A Benser, William A Hatch, James E; Analysis of off-design performance of a 16-stage axial-flow compressor with various blade modifications; naca-rm-e52l03; March 05, 1953

  119. Breitwieser, Roland Gordon, Sanford Gammon, Benson; Summary report on analytical evaluation of air and fuel specific-impulse characteristics of several nonhydrocarbon jet-engine fuels; naca-rm-e52l08; February 19, 1953

  120. Beke, Andrew Allen, J L; Force and pressure-recovery characteristics at supersonic speeds of a conical nose inlet with bypasses discharging outward from the body axis; naca-rm-e52l18a; March 05, 1953

  121. Reshotko, Eli; Preliminary investigation of a perforated axially symmetric nozzle for varying nozzle pressure ratios; naca-rm-e52j27; January 14, 1953

  122. Schramm, Wilson B Nachtigall, Alfred J Arne, Vernon L; Analytical comparison of turbine-blade cooling systems designed for a turbojet engine operating at supersonic speed and high altitude I : liquid-cooling systems; naca-rm-e52j29; February 20, 1953

  123. Schramm, Wilson B Arne, Vernon L Nachtigall, Alfred J; Analytical comparison of turbine-blade cooling systems designed for a turbojet engine operating at supersonic speed and high altitude II : air-cooling systems; naca-rm-e52j30; February 19, 1953

  124. Goldstein, Arthur W Schacht, Ralph L; Performance of a swept leading edge rotor of the supersonic type with mixed flow; naca-rm-e52k03; January 30, 1953

  125. Wallner, Lewis E Conrad, E William Prince, William R; Effect of uneven air-flow distribution to the twin inlets of an axial-flow turbojet engine; naca-rm-e52k06; January 26, 1953

  126. Trout, Arthur M Wentworth, Carl B; Free-jet altitude investigation of a 20-inch ram-jet combustor with a rich inner zone of combustion for improved low-temperature-ratio operation; naca-rm-e52l26; May 25, 1953

  127. Wise, George A; Influence of end plates on lift and flow field of a canard-type control surface at a Mach number of 2.00; naca-rm-e53a02; March 23, 1953

  128. Rebeske, John J , Jr Rohlik, Harold E; Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics I : effect of air bleed at compressor outlet; naca-rm-e53a09; March 10, 1953

  129. Bernstein, Harry Haefeli, Rudolph C; Investigation of pressure recovery of a single-conical-shock nose inlet at Mach number 5.4; naca-rm-e53a12; April 06, 1953

  130. Schafer, Louis J Stepka, Francis S Brown, W Byron; Comparison of theoretically and experimentally determined effects of oxide coatings supplied by fuel additives on uncooled turbine-blade temperature during transient turbojet-engine operation; naca-rm-e53a19; March 30, 1953

  131. Lewis, James P; An analytical study of heat requirements for icing protection of radomes; naca-rm-e53a22; March 11, 1953

  132. Freche, John C Stelpflug, William J; Investigation of water-spray cooling of turbine blades in a turbojet engine; naca-rm-e53a23; March 10, 1953

  133. Allen, J L Beke, Andrew; Force and pressure recovery characteristics at supersonic speeds of a conical spike inlet with a bypass discharging from the top or bottom of the diffuser in an axial direction; naca-rm-e53a29; March 23, 1953

  134. Jack, John R; Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) III : boundary layer and force measurements on a slender cone-cylinder body of revolution; naca-rm-e53b03; April 06, 1953

  135. Dangle, E E Cervenka, A J Bahr, D W; Effect of fuel-air ratio concentration in combustion zone on combustion performance of a 16-inch ram-jet engine; naca-rm-e53b19; April 13, 1953

  136. Kochendorfer, Fred D; Investigation at a Mach number of 1.90 of a diverter-type boundary-layer removal system for a scoop inlet; naca-rm-e53d07; June 08, 1953

  137. Krull, H George Steffen, Fred W Ciepluch, Carl C; Internal performance characteristics of variable-throat plug- and vaned-type convergent-divergent nozzles; naca-rm-e53d09; June 23, 1953

  138. Jacklitch, John J , Jr Hartmann, Melvin J; Investigation of 16-inch impulse-type supersonic compressor rotor with turning past axial direction; naca-rm-e53d13; July 06, 1953

  139. Robbins, William H Glaser, Frederick W; Investigation of an axial-flow-compressor rotor with circular-arc blades operating up to a rotor-inlet relative Mach number of 1.22; naca-rm-e53d24; July 03, 1953

  140. Cook, Preston N , Jr Evans, Vernida E Lezberg, Erwin A; Experimental investigation of physical and combustion properties of several residual fuel oils and magnesium - fuel-oil slurries in a ram-jet-type combustor; naca-rm-e53d30; June 23, 1953

  141. Rothenberg, Edward A Douglass, Howard W; Investigation of liquid fluorine : liquid ammonia propellant combination in a 100-pound-thrust rocket engine; naca-rm-e53e08; July 03, 1953

  142. Bartoo, Edward R Clure, John L; Experimental investigation of air-cooled turbine blades in turbojet engine XIII : endurance evaluation of several protective coatings applied to turbine blades of nonstrategic steels; naca-rm-e53e18; July 16, 1953

  143. Beheim, Milton A; A preliminary investigation at Mach number 1.91 of an inlet configuration designed for insensitivity to positive angle-of-attack operation; naca-rm-e53e20; July 10, 1953

  144. Nettles, J C; The effect of initial rate of subsonic diffusion on the stable subcritical mass-flow range of a conical shock diffuser; naca-rm-e53e26; July 22, 1953

  145. Branstetter, J Robert Gibbs, James B Kaufman, Warner B; Magnesium-slurry combustion performance in 6.5-inch-diameter ram-jet engine mounted in connected-pipe facility; naca-rm-e53e27; August 05, 1953

  146. Baughman, L Eugene Jack, John R; Experimental investigation of the effects of support interference on the pressure distribution of a body of revolution at a Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 14 x 10(exp 6); naca-rm-e53e28; August 05, 1953

  147. Von Glahn, U; Preliminary results of heat transfer from a stationary and rotating ellipsoidal spinner; naca-rm-e53f02; August 06, 1953

  148. Walker, Curtis L Braithwaite, Willis M Sivo, Joseph N; Altitude evaluation of several afterburner design variables on a J47-GE-17 turbojet engine; naca-rm-e53f10; October 23, 1953

  149. Fradenburgh, Evan A Kremzier, Emil J; Performance comparison of three canard-type ram-jet missile configurations at Mach numbers from 1.5 to 2.0; naca-rm-e53f11; August 14, 1953

  150. Cervenka, A J Perchonok, Eugene Dangle, E E; Effect of fuel injector location and mixture control on performance of a 16-inch ram-jet can-type combustor; naca-rm-e53f15; July 29, 1953

  151. Meyer, A J , Jr Deutsch, G C Morgan, W C; Preliminary investigation of several root designs for cermet turbine blades in turbojet engine II : root design alterations; naca-rm-e53g02; October 13, 1953

  152. Valerino, Alfred S Pennington, Donald B Vargo, Donald J; Effect of circumferential location on angle of attack performance of twin half-conical scoop-type inlets mounted symmetrically on the RM-10 body of revolution; naca-rm-e53g09; September 09, 1953

  153. Gorton, Gerald C; Investigation of translating-spike supersonic inlet as means of mass-flow control at Mach numbers of 1.5, 1.8, and 2.0; naca-rm-e53g10; October 29, 1953

  154. Tower, Leonard K Gammon, Benson E; Analytical evaluation of effect of equivalence ratio inlet-air temperature and combustion pressure on performance of several possible ram-jet fuels; naca-rm-e53g14; 1953

  155. Esgar, Jack B Richards, Hadley T; Evaluation of effects of random permeability variations on transpiration-cooled surfaces; naca-rm-e53g16; November 30, 1953

  156. Freche, John C Mckinnon, Roy A; Experimental investigation of several water-injection configurations for turbine-blade spray cooling in a turbojet engine; naca-rm-e53h06; October 08, 1953

  157. Henzel, James G , Jr Wentworth, Carl B; Free-jet investigation of a 20-inch ram-jet combustor utilizing high-heat-release pilot burner; naca-rm-e53h14; October 16, 1953

  158. Cortright, Edgar M , Jr Kochendorfer, Fred D; Jet effects on flow over afterbodies in supersonic stream; naca-rm-e53h25; November 16, 1953

  159. Cervenka, A J Dangle, E E Friedman, Robert; Effect of inlet-air temperature on performance of a 16-inch ram-jet combustor; naca-rm-e53i03; October 29, 1953

  160. Serovy, George K Robbins, William H Glaser, Frederick W; Experimental investigation of a 0.4 hub-tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers I : rotor design and over-all performance at tip speeds from 60 to 100 percent of design; naca-rm-e53i11; December 07, 1953

  161. Benser, William A; Analysis of part-speed operation for high-pressure-ratio multistage axial-flow compressors; naca-rm-e53i15; December 04, 1953

  162. Haefeli, Rudolph C Bernstein, Harry; Performance of separation nose inlets at Mach number 5.5; naca-rm-e53i23; December 1953

  163. Voit, Charles H; Investigation of a high-pressure-ratio eight-stage axial-flow research compressor with two transonic inlet stages I : aerodynamic design; naca-rm-e53i24; December 04, 1953

  164. Beheim, Milton A; A preliminary investigation at Mach number 1.91 of a diffuser employing a pivoted cone to improve operation at angle of attack; naca-rm-e53i30; December 08, 1953

  165. Geye, Richard P Voit, Charles H Budinger, Ray E; Investigation of a high-pressure-ratio eight-stage axial-flow research compressor with two transonic inlet stages II : preliminary analysis of over-all performance; naca-rm-e53j06; December 1953

  166. Morrow, John D Nelson, Robert L; Large-scale flight measurements of zero-lift drag of 10 wing-body configurations at Mach numbers from 0.8 to 1.6; naca-rm-l52d18a; January 15, 1953

  167. Mason, Homer P; Low-lift buffet characteristics obtained from flight tests of unswept thin intersecting surfaces and of thick 35 degree sweptback surfaces; naca-rm-l52h12; January 16, 1953

  168. Pendley, Robert E Bryan, Carroll R; An investigation of some factors affecting the drag of relatively large nonlifting bodies of revolution in a slotted transonic wind tunnel; naca-rm-l52h22; January 15, 1953

  169. Pendley, Robert E Milillo, Joseph R Fleming, Frank F; An investigation of three NACA 1-series nose inlets at subsonic and transonic speeds; naca-rm-l52j23; January 07, 1953

  170. Brown, Clarence A , Jr Bressette, Walter E; Flight investigation of the zero-lift of two ram-jet missile configurations at Mach numbers from 1.00 to 1.89; naca-rm-l52j24a; March 09, 1953

  171. Peck, Robert F Mitchell, Jesse L; Rocket-model investigation of longitudinal stability and drag characteristics of an airplane configuration having a 60 degree delta wing and a high unswept horizontal tail; naca-rm-l52k04a; January 05, 1953

  172. Bland, William M , Jr Marley, Edward T; A free-flight investigation at zero lift in the Mach number range between 0.7 and 1.4 to determine the effectiveness of an inset tab as a means of aerodynamically relieving aileron hinge moments; naca-rm-l52k07; January 15, 1953

  173. Hinners, Arthur H , Jr Lee, John B; Preliminary investigation of the total-pressure-recovery characteristics of a 15 degree semiangle movable-cone variable-geometry ram-jet inlet at free-jet Mach numbers of 1.62, 2.00, 2.53, and 3.05; naca-rm-l52k10; January 08, 1953

  174. Bursnall, William J; Initial flutter tests in the Langley transonic blowdown tunnel and comparison with free-flight flutter results; naca-rm-l52k14; January 07, 1953

  175. Moul, Martin T; Flight investigation of a supersonic canard missile equipped with an auxiliary damping-in-pitch control system; naca-rm-l52k14b; February 02, 1953

  176. Gillis, Clarence L Chapman, Rowe, Jr; Summary of pitch-damping derivatives of complete airplane and missile configurations as measured in flight at transonic and supersonic speeds; naca-rm-l52k20; January 22, 1953

  177. Czarnecki, K R Lord, Douglas R; Hinge-moment characteristics for several tip controls on a 60 degree sweptback delta wing at Mach number 1.61; naca-rm-l52k28; January 22, 1953

  178. Loposer, J Dan; Average skin-friction coefficients from boundary layer measurements on an ogive-cylinder body in flight at supersonic speeds; naca-rm-l52k28a; January 16, 1953

  179. Knapp, Ronald J Johnson, Wallace E; Flight measurements of pressures on base and rear part of fuselage of the Bell X-1 research airplane at transonic speeds, including power effects; naca-rm-l52l01; January 28, 1953

  180. Hatch, John E , Jr Savelle, William M; Some effects of a sonic jet exhaust on the loading over a yawed fin at a Mach number of 3.03; naca-rm-l52l02a; January 27, 1953

  181. Mcfall, John C , Jr Hollinger, James A; Longitudinal stability, control effectiveness, and drag characteristics at transonic speeds of a rocket-propelled model of an airplane configuration having an unswept tapered wing of aspect ratio 3.0 and NACA 65A004.5 airfoil sections; naca-rm-l52l04; January 20, 1953

  182. Robinson, Harold L; A transonic wind-tunnel investigation of the effects of body indentation, as specified by the transonic drag-rise rule, on the aerodynamic characteristics and flow phenomena of a 45 degree sweptback-wing-body combination; naca-rm-l52l12; February 09, 1953

  183. Estabrooks, Bruce B; A transonic wind-tunnel investigation of an unswept-wing-body combination at angles of attack up to 24 degrees; naca-rm-l52l19; February 06, 1953

  184. Kelly, Thomas C; Transonic wind-tunnel investigation of the aerodynamic characteristics of a 60 degrees triangular wing in combination with a systematic series of three bodies; naca-rm-l52l22a; April 06, 1953

  185. Williams, Claude V; A transonic wind-tunnel investigation of the effects of body indentation, as specified by the transonic drag-rise rule, on the aerodynamic characteristics and flow phenomena of an unswept-wing-body combination; naca-rm-l52l23; January 28, 1953

  186. Katzoff, S Smith, Samuel L , III; A theoretical analysis of the distortion of fuel-spray-particle paths in a helicopter ram-jet engine due to centrifugal effects; naca-rm-l53a02; April 07, 1953

  187. Arbic, Richard G White, George Gillespie, Warren, Jr; Some approximate methods for estimating the effects of aeroelastic bending of rocket-propelled model-booster combinations; naca-rm-l53a08; March 27, 1953

  188. Mcdearmon, Russell W Heinke, Harry S , Jr; Investigations of the damping in roll of swept and tapered wings at supersonic speeds; naca-rm-l53a13; March 03, 1953

  189. Sevier, John R , Jr Hamilton, Clyde V Driver, Cornelius; Wind-tunnel investigation of a ram-jet missile model having a wing and canard surfaces of delta plan form with 70 degrees swept leading edges : force and moment characteristics of various combinations of components at a Mach number of 1.6; naca-rm-l53a14; March 09, 1953

  190. Osborne, Robert S Kelly, Thomas C; A note on the drag due to lift of delta wings at Mach numbers up to 2.0; naca-rm-l53a16a; April 09, 1953

  191. Harrison, Daniel E; The influence of a change in body shape on the effects of twist and camber as determined by a transonic wind-tunnel investigation of a 45 degree sweptback wing-fuselage configuration; naca-rm-l53b03; August 14, 1953

  192. Kindell, William H; Effects of span and spanwise and chordwise location on the control effectiveness of spoilers on a 50 degree sweptback wing at Mach numbers of 1.41 and 1.96; naca-rm-l53b09; April 08, 1953

  193. Johnson, Harold S Hayes, William C; Wind-tunnel investigation of the effects of various dorsal-fin and vertical-tail configurations on the directional stability of a streamlined body at transonic speeds : transonic-bump method; naca-rm-l53b19; April 08, 1953

  194. Czarnecki, K R Sinclair, Archibald R; An extension of the investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61; naca-rm-l53b25; March 26, 1953

  195. Wallskog, Harvey A Morrow, John D; Large-scale flight measurements of zero-lift drag and low-lift longitudinal characteristics of a diamond-wing-body combination at Mach numbers from 0.725 to 1.54; naca-rm-l53c17; April 20, 1953

  196. Kurbjun, Max C Thompson, Jim Rogers; Free-fall measurements of the effects of wing-body interference on the transonic drag characteristics of swept-wing-slender-body configurations; naca-rm-l53c31; May 28, 1953

  197. Carpenter, Paul J Radin, Edward J; Investigation of a ram-jet-powered helicopter rotor on the Langley helicopter test tower; naca-rm-l53d02; June 03, 1953

  198. Dunning, Robert W Ulmann, Edward F; Aerodynamic characteristics at Mach number 4.04 of a rectangular wing of aspect ratio 1.33 having a 6-percent-thick circular-arc profile and a 30-percent-chord full-span trailing-edge flap; naca-rm-l53d03; May 29, 1953

  199. Goin, Kennith L Westrick, Gertrude C; Effects of trailing-edge bluntness on the lift, drag, and pitching-moment characteristics of unswept, 45 degree swept, and 45 degree delta wings at Mach numbers of 1.41, 1.62, and 1.96; naca-rm-l53d13; June 10, 1953

  200. Czarnecki, K R Lord, Douglas R; Preliminary investigation of the effect of fences and balancing tabs on the hinge-moment characteristics of a tip control on a 60 degree delta wing at Mach number 1.61; naca-rm-l53d14; May 29, 1953

  201. Wallskog, Harvey A Hart, Roger G; Investigation of the drag of blunt-nosed bodies of revolution in free flight at Mach numbers from 0.6 to 2.3; naca-rm-l53d14a; June 11, 1953

  202. Czarnecki, K R Lord, Douglas R; Load distributions associated with controls at supersonic speeds; naca-rm-l53d15a; May 29, 1953

  203. Vogler, Raymond D; Wind-tunnel investigation at high subsonic speeds of a spoiler-slot deflector combination on an NACA 65A006 wing with quarter-chord line swept back 32.6 degrees; naca-rm-l53d17; May 29, 1953

  204. Johnson, Harold I; Measurements of aerodynamic characteristics at transonic speeds of an unswept and untapered NACA 65-009 airfoil model of aspect ratio 3 with 1/4-chord plain flap by the NACA wing-flow method; naca-rm-l53d21; June 10, 1953

  205. Rainey, Robert W; Effect of variations in Reynolds number on the aerodynamic characteristics of three bomb or store shapes at a Mach number of 1.62 with and without fins; naca-rm-l53d27; June 25, 1953

  206. Carter, Howard S Merlet, Charles F; Flight determination of the pressure recovery and drag characteristics of a twin side-inlet model at transonic speeds; naca-rm-l53e05; July 30, 1953

  207. Cooper, Morton Sevier, John R , Jr; Effects of a series of inboard plan-form modifications on the longitudinal characteristics of two 47 degree sweptback wings of aspect ratio 3.5, taper ratio 0.2, and different thickness distributions at Mach numbers of 1.61 and 2.01; naca-rm-l53e07a; July 17, 1953

  208. Williams, Claude V Kuhn, Richard E; A study of the aerodynamic loads on sweptback wings at transonic speeds; naca-rm-l53e08b; June 25, 1953

  209. Dettwyler, H Rudolph Faget, Maxime A; Engineering method of ram-jet thrust determination based on experimentally obtained combustor parameters; naca-rm-l53e21; August 13, 1953

  210. Williams, Claude V; A transonic wind-tunnel investigation of the effects of body indentation on the aerodynamic characteristics of an approximate-delta-wing-body configuration, and a comparison with a wing of reversed plan form; naca-rm-l53f05a; August 13, 1953

  211. Dennard, John S; A preliminary investigation of the power requirements of slotted test sections; naca-rm-l53f10; July 07, 1953

  212. Nelson, William J Vick, Allen R; Slotted-boundary interference effects on wedge airfoils at low supersonic Mach numbers; naca-rm-l53f11; July 30, 1953

  213. Arbic, Richard G Gillespie, Warren, Jr; Free-flight longitudinal-stability investigation including some effects of wing elasticity from Mach numbers of 0.85 to 1.34 of a tailless missile configuration having a 45 degree sweptback wing of aspect ratio 5.5; naca-rm-l53f18; August 10, 1953

  214. Pendley, Robert E Milillo, Joseph R Fleming, Frank F Bryan, Carroll R; An experimental study of five annular air inlet configurations at subsonic and transonic speeds; naca-rm-l53f18a; August 19, 1953

  215. Palmer, William E; Effect of reduction in thickness from 6 to 2 percent and removal of the pointed tips on the subsonic static longitudinal stability characteristics of a 60 degree triangular wing in combination with a fuselage; naca-rm-l53f24; August 19, 1953

  216. Savage, Melvyn Erwin, John R Whitley, Robert P; Investigation of an axial-flow compressor rotor having NACA high-speed blade sections (A(sub 2)I(sub 8b) series) at mean radius relative inlet Mach numbers up to 1.13; naca-rm-l53g02; November 30, 1953

  217. Carlson, Harry W; Preliminary investigation of the effects of body contouring as specified by the transonic area rule on the aerodynamic characteristics of a delta wing-body combination at Mach numbers of 1.41 and 2.01; naca-rm-l53g03; September 22, 1953

  218. Solomon, William West, F E , Jr Brummal, Edward M; Investigation of spoiler ailerons with and without a gap behind the spoiler on a 45 degree sweptback wing-fuselage combination at Mach numbers from 0.60 to 1.03; naca-rm-l53g07a; September 14, 1953

  219. Wiggins, James W; Wind-tunnel investigation at high subsonic speeds of the static longitudinal and static lateral stability characteristics of a wing-fuselage combination having a triangular wing of aspect ratio 2.31 and an NACA 65A003 airfoil; naca-rm-l53g09a; August 28, 1953

  220. Jones, George W , Jr Dubose, Hugh C; Investigation of wing flutter at transonic speeds for six systematically varied wing plan forms; naca-rm-l53g10a; August 13, 1953

  221. (Author(s) Not Available); Notes on damping in roll and load distributions in roll at high angles of attack and high subsonic speed; naca-rm-l53g13a; August 27, 1953

  222. Passera, Anthony L Nason, Martin L; The effect of control-surface-servo natural frequency on the dynamic performance characteristics of an acceleration control system applied to a supersonic missile; naca-rm-l53g23a; September 29, 1953

  223. Moul, Martin T Baber, Hal T , Jr; Flight investigation at Mach numbers from 0.67 to 1.81 of the longitudinal stability and control characteristics of a 60 degree delta-wing missile configuration having an all-movable tail; naca-rm-l53g29; October 06, 1953

  224. Kemp, William B , Jr Becht, Robert E; Damping-in-pitch characteristics at high subsonic and transonic speeds of four 35 degree sweptback wings; naca-rm-l53g29a; October 16, 1953

  225. Yeates, John E , Jr Thompson, Jim Rogers; A preliminary study by means of electrical frequency-analysis techniques of the response of an airplane structure during buffeting; naca-rm-l53g31; December 08, 1953

  226. Goin, Kennith L Palmer, William E; Subsonic and supersonic hinge-moment and effectiveness characteristics of an unbalanced lateral control having low theoretical hinge moments at supersonic speeds; naca-rm-l53g31a; October 19, 1953

  227. Swihart, John M Whitcomb, Charles F; Pressure distributions on three bodies of revolution to determine the effect of Reynolds number up to and including the transonic speed range; naca-rm-l53h04; October 15, 1953

  228. O'Sullivan, William J Rumsey, Charles B Chauvin, Leo T; Exploratory investigation of transpiration cooling to alleviate aerodynamic heating on an 8 degree cone in a free jet at a Mach number of 2.05; naca-rm-l53h06; September 14, 1953

  229. Strass, H Kurt Stephens, Emily W; An engineering method for the determination of aeroelastic effects upon the rolling effectiveness of ailerons on swept wings; naca-rm-l53h14; November 30, 1953

  230. Radin, Edward J Carpenter, Paul J; Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings; naca-rm-l53h18a; October 07, 1953

  231. Ogburn, Edmund L Grigsby, Carl E; Investigation of Reynolds number effects for a series of cone-cylinder bodies at Mach numbers of 1.62, 1.93, and 2.41; naca-rm-l53h21; October 07, 1953

  232. Henderson, Arthur, Jr; Investigation at Mach numbers of 1.62, 1.93, and 2.41 of the effect of oscillation amplitude on the damping in pitch of delta-wing-body combinations; naca-rm-l53h25; October 26, 1953

  233. Strass, H Kurt Marley, Edward T; Recent experiences with flutter failure of sweptback, tapered wings having outboard, partial-span spoiler controls; naca-rm-l53h26; October 05, 1953

  234. Hinners, Arthur H , Jr Foland, Douglas, H; Preflight tests and flight performance of a 6.5-inch diameter ram-jet engine; naca-rm-l53h28; November 02, 1953

  235. Stoney, William E , Jr; Some experimental effects of afterbody shape on the zero-lift drag of bodies for Mach numbers between 0.8 and 1.3; naca-rm-l53i01; October 1953

  236. Spearman, M Leroy; Component tests to determine the aerodynamic characteristics of an all-moveable 70 degree delta canard-type control in the presence of a body at a Mach number of 1.61; naca-rm-l53i03; October 09, 1953

  237. Martz, C William Goslee, John W; Rocket-model investigation to determine the hinge-moment and normal-force properties of a full-span, constant-chord, partially balanced trailing-edge control on a 60 degree clipped delta wing between Mach numbers of 0.50 and 1.26; naca-rm-l53i04; October 30, 1953

  238. Hatch, John E , Jr Gallagher, James J; Aerodynamic characteristics of a 68.4 degree delta wing at Mach numbers of 1.6 and 1.9 over a wide Reynolds number range; naca-rm-l53i08; November 02, 1953

  239. Gardiner, Robert A; A combined aerodynamic and guidance approach for a simple homing system; naca-rm-l53i10a; November 02, 1953

  240. Spearman, M Leroy; Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a Mach number of 2.01; naca-rm-l53i14; October 30, 1953

  241. Hasel, Lowell E; The performance of conical supersonic scoop inlets on circular fuselages; naca-rm-l53i14a; November 17, 1953

  242. Lord, Douglas R Czarnecki, K R; Recent information on flap and tip controls; naca-rm-l53i17a; November 17, 1953

  243. Robins, A Warner; Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60; naca-rm-l53i18; October 30, 1953

  244. Mueller, James N; An investigation at Mach number 2.40 of flap-type controls equipped with overhang nose balances; naca-rm-l53i21; November 17, 1953

  245. Curfman, Howard J , Jr Strass, H Kurt Crane, Harold L; Investigations toward simplification of missile control systems; naca-rm-l53i21a; November 12, 1953

  246. Toll, Thomas A; Longitudinal characteristics of wings; naca-rm-l53i21b; October 28, 1953

  247. Sternfield, Leonard; Several factors affecting roll control systems of interceptors; naca-rm-l53i22a; November 06, 1953

  248. Gapcynski, John P Robins, A Warner; The effect of nose radius and shape on the aerodynamic characteristics of a fuselage and a wing-fuselage combination at angles of attack; naca-rm-l53i23a; October 22, 1953

  249. Weil, Joseph Gray, W H; Recent design studies directed toward elimination of pitch-up; naca-rm-l53i23c; November 18, 1953

  250. Lowry, John G; Data on spoiler-type ailerons; naca-rm-l53i24a; October 28, 1953

  251. English, Roland D; Some effects of leading-edge roughness on the aileron effectiveness and drag of a thin rectangular wing employing a full-span plain aileron at Mach numbers from 0.6 to 1.5; naca-rm-l53i25; November 04, 1953

  252. Sears, R I Merlet, C F Putland, L W; Flight determination of drag of normal-shock nose inlets with various cowling profiles at Mach numbers from 0.9 to 1.5; naca-rm-l53i25a; October 22, 1953

  253. Henning, Allen B; Results of a rocket-model investigation of control-surface buzz and flutter on a 4-percent-thick unswept wing and on 6-, 9-, and 12-percent-thick swept wings at transonic speeds; naca-rm-l53i29; November 20, 1953

  254. Johnson, Harold S; Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination with quarter-chord line swept back 32.6 degrees and NACA 65A006 airfoil section; naca-rm-l53j05a; November 20, 1953

  255. Morris, Odell A; Control hinge-moment and effectiveness characteristics of several interchangeable tip controls on a 60 degree delta wing at Mach numbers of 1.41, 1.62, and 1.96; naca-rm-l53j08a; November 25, 1953

  256. Johnson, Harold S; Wind-tunnel investigation at low speed of the effect of varying the ratio of body diameter to wing span from 0.1 to 0.8 on the aerodynamic characteristics in pitch of a 45 degree sweptback-wing-body combination; naca-rm-l53j09a; November 30, 1953

  257. Parks, James H Kehlet, Alan B; Longitudinal stability and trim of two rocket propelled airplane models having 45 degree sweptback wings and tails with the horizontal tail mounted in two positions; naca-rm-l53j12a; December 09, 1953

  258. Passera, Anthony L Bridgland, Thomas F , Jr; The influence of the control-surface-servo natural frequency upon the transient characteristics of a flight-path-angle control system incorporating a supersonic missile; naca-rm-l53j15; December 10, 1953

  259. Wiley, Harleth G Riley, Donald R; An experimental and theoretical investigation at high subsonic speeds of the effects of horizontal-tail height on the aerodynamic characteristics of an unswept, untapered tail assembly; naca-rm-l53j19; December 02, 1953

  260. Vogler, Raymond D; Wind-tunnel investigation at transonic speeds of a spoiler-slot-deflector combination on an unswept NACA 65A006 wing; naca-rm-l53j21; December 08, 1953

  261. Mason, Homer P; Effects of external store mounting on the buffet, trim, and drag characteristics of rocket-powered fuselage and store combinations between Mach numbers of 0.7 and 1.4; naca-rm-l53j22; December 10, 1953

  262. Spearman, M Leroy; Effect of large deflection of a canard control and deflections of a wing-tip control on the static-stability and induced-roll characteristics of a cruciform canard missile at a Mach number of 2.01; naca-rm-l53k03; December 14, 1953

  263. Houbolt, John C; Correlation of calculation and flight studies of the effect of wing flexibility on structural response due to gusts; naca-tn-3006; August 1953

  264. Diederich, Franklin W Zlotnick, Martin; Calculated spanwise lift distributions and aerodynamic influence coefficients for unswept wings in subsonic flow; naca-tn-3014; September 1953

  265. Garrick, I E Watkins, C E; A theoretical study of the effect of forward speed on the free-space sound-pressure field around propellers; naca-tn-3018; October 1953

  266. Amer, Kenneth B; Method for studying helicopter longitudinal maneuver stability; naca-tn-3022; October 1953

  267. Gray, W L (Boeing Airplane Company) Schenk, K M (Boeing Airplane Company); A method for calculating the subsonic steady-state loading on an airplane with a wing of arbitrary plan form and stiffness; naca-tn-3030; December 1953

  268. Liepmann, H W (California Institute of Technology) Robinson, M S (California Institute of Technology); Counting methods and equipment for mean-value measurements in turbulence research; naca-tn-3037; October 1953

  269. Walker, Walter G; Summary of revised gust-velocity data obtained from V-G records taken on civil transport airplanes from 1933 to 1950; naca-tn-3041; November 1953

  270. Hickman, William A Dow, Norris F; Direct-reading design charts for 24S-T3 aluminum-alloy flat compression panels having longitudinal formed hat-section stiffeners and comparisons with panels having z-section stiffeners; naca-tn-2792; March 1953

  271. Leonard, Robert W Budiansky, Bernard; On traveling waves in beams; naca-tn-2874; 1953

  272. Wilder, Thomas W , III; An analysis of statically indeterminate trusses having members stressed beyond the proportional limit; naca-tn-2886; February 1953

  273. Das, Dilip K (University of Notre Dame) Beck, Paul A (University of Notre Dame); Survey of portions of the iron-nickel-molybdenum and cobalt-iron-molybdenum ternary systems at 1200 C; naca-tn-2896; February 1953

  274. Castles, Walter, Jr (Georgia Institute of Technology) De Leeuw, Jacob Henri (Georgia Institute of Technology); The normal component of the induced velocity in the vicinity of a lifting rotor and some examples of its application; naca-tn-2912; March 1953

  275. Callaghan, Edmund E Serafini, John S; A method for rapid determination of the icing limit of a body in terms of the stream conditions; naca-tn-2914; March 1953

  276. Grover, H J (Battelle Memorial Institute) Hyler, W S (Battelle Memorial Institute) Kuhn, Paul (Aluminum Company of America) Landers, Charles B Howell, F M; Axial-load fatigue properties of 24S-T and 75S-T aluminum alloy as determined in several laboratories; naca-tn-2928; May 1953

  277. Stokes, George M Davis, Don D , Jr; The attenuation characteristics of four specially designed mufflers tested on a practical engine setup; naca-tn-2943; May 1953

  278. Skopinski, T H Aiken, William S , Jr Huston, Wilber B; Calibration of strain-gage installations in aircraft structures for the measurements of flight loads; naca-tn-2993; August 1953

  279. Eggleston, John M Mathews, Charles W; Application of several methods for determining transfer functions and frequency response of aircraft from flight data; naca-tn-2997; September 1953

  280. Wolock, I (National Bureau of Standards) Axilrod, B M (National Bureau of Standards) Sherman, M A (National Bureau of Standards); Effects of high degrees of biaxial stretch forming on crazing and other properties of acrylic plastic glazing; naca-rm-53d14; June 29, 1953

  281. Smith, Willard G; Wind-tunnel investigation at subsonic and supersonic speeds of a model of a tailless fighter airplane employing a low-aspect-ratio swept-back wing : effects of external fuel tanks and rocket packets on the drag characteristics; naca-rm-a52j31; January 12, 1953

  282. Rolls, L Stewart Havill, C Dewey Holden, George R; Techniques for determining thrust in flight for airplanes equipped with afterburners; naca-rm-a52k12; January 19, 1953

  283. Franks, Ralph W; Tests in the Ames 40- by 80-foot wind tunnel of an airplane model with an aspect ratio 4 triangular wing and an all-movable horizontal tail - high-lift devices and lateral controls; naca-rm-a52k13; February 20, 1953

  284. Hightower, Ronald C; Lift, drag and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : comparison of three wings of aspect ratio 2 of rectangular, swept-back and triangular plan form, including effects of thickness distribution; naca-rm-a52l02; February 16, 1953

  285. Franks, Ralph W; Tests in the Ames 40- by 80-foot wind tunnel of two airplane models having aspect ratio 2 trapezoidal wings of taper ratios 0.33 and 0.20; naca-rm-a52l16; February 16, 1953

  286. Anderson, Seth B Van Dyke, Rudolph D , Jr Matteson, Frederick H; A flight investigation of the effect of leading-edge camber on the aerodynamic characteristics of a swept-wing airplane; naca-rm-a52l16a; February 18, 1953

  287. Rolls, L Stewart; A flight comparison of a submerged inlet and a scoop inlet at transonic speeds; naca-rm-a53a06; March 19, 1953

  288. Gowen, Forrest E; Buffeting of a vertical tail on an inclined body at supersonic Mach numbers; naca-rm-a53a09; March 24, 1953

  289. Hopkins, Edward J Carel, Hubert C; Experimental and theoretical study of the interference at low speed between slender bodies and triangular wings; naca-rm-a53a14; May 06, 1953

  290. James, Harry A Mcfadden, Norman M Mccloud, John L , III; Comparison of measured and predicted indicated angles of attack near the fuselages of a triangular-wing wind-tunnel model and a swept-wing fighter airplane in flight; naca-rm-a53a15; March 11, 1953

  291. Reynolds, Robert M Sammonds, Robert I Kenyon, George C; An investigation of a four-blade single-rotation propeller in combination with an NACA 1-series D-type cowing at Mach numbers up to 0.83; naca-rm-a53b06; April 13, 1953

  292. Matthews, Howard F Schmidt, Stanley F; A theoretical study of the effect of control-deflection and control-rate limitations on the normal acceleration and roll response of a supersonic interceptor; naca-rm-a53b11; April 29, 1953

  293. Tinling, Bruce E Lopez, Armando E; The effects of nacelles and of extended split flaps on the longitudinal characteristics of a wing-fuselage-tail combination having a wing with 40 degrees of sweepback and an aspect ratio of 10; naca-rm-a53d06; June 05, 1953

  294. Graham, David; The low-speed lift and drag characteristics of a series of airplane models having triangular or modified triangular wings; naca-rm-a53d14; June 15, 1953

  295. Koenig, David G; Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with a variable-incidence triangular wing and an all-movable horizontal tail; naca-rm-a53d21; June 25, 1953

  296. Holzhauser, Curt A Cook, Woodrow L Kelly, Mark W; The use of area suction for the purpose of improving trailing-edge flap effectiveness on a 35 degree sweptback wing; naca-rm-a53e06; July 02, 1953

  297. Selan, Ralph Bandittini, Angelo; The effects of leading-edge extensions, a trailing-edge extension, and a fence on the static longitudinal stability of a wing-fuselage-tail combination having a wing with 35 degrees of sweepback and an aspect ratio of 4.5; naca-rm-a53e12; August 07, 1953

  298. Abramovitz, Marvin Schmidt, Stanley F Van Dyke, Rudolph D , Jr; Investigation of the use of a stick force proportional to pitching acceleration for normal-acceleration warning; naca-rm-a53e21; August 14, 1953

  299. Reed, Verlin D Smith, Donald W; The lateral control characteristics of constant-percent-chord trailing-edge elevons on a pointed wing of aspect ratio 2 at Mach numbers up to 0.95; naca-rm-a53f03; August 14, 1953

  300. Drake, William C; Lift, drag, and hinge moments at supersonic speeds of an all-movable triangular wing and body combination; naca-rm-a53f22; September 16, 1953

  301. Bray, Richard S; The effects of fences on the high-speed longitudinal stability of a swept-wing airplane; naca-rm-a53f23; August 31, 1953

  302. Hemenover, Albert D; Tests of the NACA 0010-1.50 40/1.051 airfoil section at high subsonic Mach numbers; naca-rm-a53g09; September 04, 1953

  303. Sadoff, Melvin; Flight measurements of the horizontal-tail loads on a swept-wing fighter airplane at transonic speeds; naca-rm-a53g10; November 06, 1953

  304. Anderson, Seth B; Correlation of flight and wind-tunnel measurements of roll-off in low-speed stalls on a 35 degree swept-wing aircraft; naca-rm-a53g22; September 24, 1953

  305. Ziff, Howard L Rathert, George A Gadeberg, Burnett L; An analysis of the tracking performances of two straight-wing and two swept-wing fighter airplanes with fixed sights in a standardized test maneuver; naca-rm-a53h12; October 22, 1953

  306. Spiegel, Joseph M Kuehn, Donald M Hofstetter, Robert U; Applications of auxiliary air injectors to supersonic wind tunnels; naca-rm-a53i01; November 25, 1953

  307. Cleary, Joseph W Boddy, Lee E; Wind-tunnel investigation of a 45 degree sweptback wing having a symmetrical root and a highly cambered tip, including the effects of fences and lateral controls; naca-rm-a53i21; November 20, 1953

  308. Axelson, John A; Downwash behind a triangular wing of aspect ratio 3 - : transonic bump method; naca-rm-a53i23; December 1953

  309. Holzhauser, Curt A Martin, Robert K; The use of a leading-edge area-suction flap to delay separation of air flow from the leading edge of a 35 degrees sweptback wing; naca-rm-a53j26; December 10, 1953

  310. Zlotnick, Martin Robinson, Samuel W , Jr; A simplified mathematical model for calculating aerodynamic loading and downwash for midwing wing-fuselage combinations with wings of arbitrary plan form; naca-rm-l52j27a; January 16, 1953

  311. Newman, Ernest E Cahill, Jones F; Investigation at low speed of the flow field behind the lifting surfaces of a model equipped with a 60 degree triangular wing and a 60 degree triangular canard tail; naca-rm-l53c30; June 29, 1953

  312. Fournier, Paul G; Wind-tunnel investigation of the aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a wing fuselage combination having a triangular wing of aspect ratio 4; naca-rm-l53g14a; August 28, 1953

  313. Trimpi, Robert L; A theory for stability and buzz pulsation amplitude in ram jets and an experimental investigation including scale effects; naca-rm-l53g28; October 15, 1953

  314. Cahen, George L; Gust-tunnel investigation of the effect of leading edge separation on the normal accelerations experienced by a 45 degree sweptback-wing model in gusts; naca-rm-l53j07; November 24, 1953

  315. Sretensky, L. N.; Motion of a cylinder under the surface of a heavy fluid; naca-tm-1335; 1953

  316. Hamel, Georg.; Spiral motions of viscous fluids; naca-tm-1342; 1953

  317. Rotta, J.; On the theory of the turbulent boundary layer; naca-tm-1344; 1953

  318. Schlichting, Hermann., Moller, Egon.; Report on the special field "Interference" to the wind-tunnel committee in February 1945; naca-tm-1347; 1953

  319. Yatseyev, V. I.; On a class of exact solutions of the equations of motion of a viscous fluid; naca-tm-1349; 1953

  320. Obukhoff, A. M., Yaglom, A. M.; The microstructure of turbulent flow; naca-tm-1350; 1953

  321. Rabotnov, Y. N.; Some problems on the theory of creep; naca-tm-1353; 1953

  322. Fabri, Jean., Siestrunck, Raymond.; Study of the supersonic propeller; naca-tm-1355; 1953

  323. Sanger, Eugen.; Air admixture to exhaust jets; naca-tm-1357; 1953

  324. Fradenburgh, Evan A., Campbell, Robert C.; Characteristics of a canard-type missile configuration with an underslung scoop inlet at Mach numbers from 1.5 to 2.0; naca-rm-e52j22; 1953

  325. Love, Eugene S.; Base pressure at supersonic speeds on two-dimensional airfoils and on bodies of revolution (with and without fins) having turbulent boundary layers; naca-rm-l53c02; 1953

  326. Allen, H. Julian, Eggers, A. J. Jr.; A study of the motion and aerodynamic heating of missiles entering the earth's atmosphere at high supersonic speeds; naca-rm-a53d28; 1953

  327. Weick, Fred E (Agricultural and Mechanical College of Texas) Sevelson, Maurice S (Agricultural and Mechanical College of Texas) Mcclure, James G (Agricultural and Mechanical College of Texas) Flanagan, Marion D (Agricultural and Mechanical College of Texa; Investigation of lateral control near the stall flight investigation with a light high-wing monoplane tested with various amounts of washout and various lengths of leading-edge slot; naca-tn-2948; May 1953

  328. Vasu, George., Hinde, William L.; Effect of engine and control limits on steady-state and transient performance of turbojet engine with variable-area exhaust nozzle; naca-rm-e52e23; 1953

  329. Gabriel, David S., Krebs, Richard P., Wilcox, E. Clinton., Koutz, Stanley L.; Analysis of the turbojet engine for propulsion of supersonic fighter airplanes / David S. Gabriel, Richard P. Krebs, E.Clinton Wilcox, Stanley L.Koutz; naca-rm-e52f17; 1953

  330. Finger, Harold B., Essig, Robert H., Conrad, E. William.; Effect of rotor-and stator-blade modifications on surge performance of an 11-stage axial-flow compressor I :original production compressor of XJ40-WE-6 engine; naca-rm-e52g03; 1953

  331. Renas, Paul E., Jansen, Emmert T.; Altitude performance characteristics of the J47-25 turbojet engine :data presentation; naca-rm-e52g22; 1953

  332. Bloomer, Harry E., Walker, William J., Pantages, George L.; Altitude investigation of XJ34-WE-32 engine performance without electronic control; naca-rm-e51l12; 1953

  333. Smith, Willard G.; Wind-tunnel investigation at subsonic and supersonic speeds of a model of a tailless fighter airplane employing a low-aspect-ratio swept-back wing :stability and control; naca-rm-a52j30; 1953

  334. Reynolds, Robert M.; Preliminary results of an investigation of the effects of spinner shape on the characteristics of an NACA D-type cowl behind a three-blade propeller, including the characteristics of the propeller at negative thrust; naca-rm-a53j02; 1953

  335. Calvert, Howard F., Meyer, Andre' J., Jr., Morse, C. Robert.; Investigation of blade failures in a J34, eleven-stage axial-flow compressor; naca-rm-e52i16; 1953

  336. Bogart, Donald., Valerino, Michael F.; The sodium hydroxide reactor :effect of reactor variables on criticality and fuel-element temperature requirements for subsonic and supersonic aircraft nuclear propulsion; naca-rm-e52i19; 1953

  337. Ladanyi, Dezso J., Miller, Riley O., Karo, Wolf., Feiler, Charles E.; Some fundamental aspects of nitric acid oxidants for rocket applications; naca-rm-e52j01; 1953

  338. Sobolewski, Adam E., Miller, Robert R., McAulay, John E.; Altitude performance investigation of two single-annular type combustors and the prototype J40-WE-8 turbojet engine combustor with various combustor-inlet air pressure profiles; naca-rm-e52j07; 1953

  339. Norgren, Carl T., Childs, J. Howard.; Effect of liner air-entry holes, fuel state, and combustor size on performance of an annular turbojet combustor at low pressures and high air-flow rates; naca-rm-e52j09; 1953

  340. Campbell, Carl E., Welna, Henry J.; Preliminary evaluation of turbine performance with variable-area turbine nozzles in a turbojet engine; naca-rm-e52j20; 1953

  341. Foster, Hampton H., Straight, David M.; Effect of fuel volatility characteristics on ignition-energy requirements in a turbojet combustor; naca-rm-e52j21; 1953

  342. Farley, John M., Smith, Robert E., Povolny, John H.; Preliminary experiments with pilot burners for ram-jet combustors; naca-rm-e52j23; 1953

  343. Dugger, Gordon L., Graab, Dorothy D.; Flame velocities of propane- and ethylene-oxygen-nitrogen mixtures; naca-rm-e52j24; 1953

  344. Fleming, William A.; Internal performance of several types of jet-exit configurations for supersonic turbojet aircraft; naca-rm-e52k04; 1953

  345. DiPiazza, J. T.; A compilation of summaries from NACA reports on fuels research, 1945-1952; naca-rm-53d28; 1953

  346. Smith, Gordon T., Curren, Arthur N.; Comparison of pressure-loss characteristics of several tail-cone air-induction systems for air-cooled gas-turbine rotors; naca-rm-e52k07; 1953

  347. McAulay, John E., Kaufman, Harold R.; Altitude wind tunnel investigation of the prototype J40-WE-8 turbojet engine without afterburner; naca-rm-e52k10; 1953

  348. Lord, Albert M., Evans, Vernida E.; Effect of particle size and stabilizing additives on the combustion properties of magnesium slurry; naca-rm-e52k12; 1953

  349. Deutsch, George C., Meyer, Andre J., Jr., Morgan, William C.; Preliminary investigation in J33 turbojet engine of several root designs for ceramal turbine blades; naca-rm-e52k13; 1953

  350. Hollister, Donald P., Greathouse, William K.; Performance of double-shroud ejector configuration with primary pressure ratios from 1.0 to 10; naca-rm-e52k17; 1953

  351. Ladanyi, Dezso J.; Orthotoluidine and triethylamine in rocket engine applications; naca-rm-e52k19; 1953

  352. Miller, Riley O.; Ignition delays of some nonaromatic fuels with low-freezing red fuming nitric acid in temperature range -40 to -105 F; naca-rm-e52k20; 1953

  353. Miller, Riley O., Ladanyi, Dezso J.; Ignition delays of alkyl thiophosphites with white and red fuming nitric acids within temperature range 80 to -105 F; naca-rm-e52k25; 1953

  354. Macks, E. Fred., Anderson, W. J., Nemeth, Zolton N.; Preliminary comparison of 17- and 75-millimeter-bore cageless cylindrical roller bearings with conventional cylindrical roller bearings at high speeds; naca-rm-e52l05; 1953

  355. Grele, Milton D., Gedeon, Louis.; Forced-convection heat-transfer characteristics of molten sodium hydroxide; naca-rm-e52l09; 1953

  356. Conrad, E. William., Campbell, Carl E.; Altitude investigation of several afterburner configurations for the J40-WE-8 turbojet engine; naca-rm-e52l10; 1953

  357. Gordon, Sanford., Huff, Vearl N.; Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant; naca-rm-e52l11; 1953

  358. Jansen, E. T., Renas, P. E.; Altitude investigation of thrust augmentation using water-alcohol injection into the combustion chambers of an axial-flow turbojet engine; naca-rm-e52l12; 1953

  359. Hoffman, Charles A.; Preliminary investigation of zirconium boride ceramals for gas-turbine blade applications; naca-rm-e52l15a; 1953

  360. Walker, Curtis L., Braithwaite, Willis M., Fenn, David B.; Component and over-all performance evaluation of a J47-GE-25 turbojet engine over a range of engine-inlet Reynolds number indices; naca-rm-e52l16; 1953

  361. Garrett, Floyd B., Gyorgak, Charles A., Weeton, John Waldemar.; Behavior of forged S-816 turbine blades in steady-state operation of J33-9 turbojet engine with stress-rupture and metallographic evaluations / By F. B.Garrett, C. A. Gyorgak, and J. W. Weeton; naca-rm-e52l17; 1953

  362. Maxwell, W. A.; Preliminary investigation of plate-type molybdenum disilicide fuel elements for an air-cycle nuclear reactor; naca-rm-e52l18; 1953

  363. Useller, James W., Fenn, David B., Harp, James L., Jr.; Turbojet-engine thrust augmentation at altitude by combined ammonia injection into the compressor inlet and afterburning; naca-rm-e52l19; 1953

  364. Nagey, T. F., Sams, E. W.; Effect of drawbar upstream location on air velocity distribution at the inlet face of reactor segment designed by the General Electric Company; naca-rm-e52l22; 1953

  365. Lowell, Herman H.; Free fall and evaporation of N-Octane droplets in the atmosphere as applied to the jettisoning of aviation gasoline at altitude; naca-rm-e52l23a; 1953

  366. Hansen, Arthur G., Costello, George R., Herzig, Howard Z.; Smoke studies of secondary flows in bends, tandem cascades, and high-turning configurations; naca-rm-e52l24a; 1953

  367. Garrett, Floyd B., Gyorgak, Charles A.; Adhesive and protective characteristics of ceramic coating A-417 and its effect on engine life of forged Refractaloy-26 (AMS 5760) and cast stellite 21 (AMS 5385) turbine blades; naca-rm-e52l30; 1953

  368. Yeomans, C. M., Hoffman, C. A.; Thermal-shock resistance of a ceramic comprising 60 percent boron carbide and 40 percent titanium diboride; naca-rm-e52l31; 1953

  369. Robert W. Dunning and Fred M. Smith (Langley Aeronautical Laboratory, Langley Field, Va.); Aerodynamic Characteristics of Two Delta Wings and Two Trapezoidal Wings at Mach Number 4.04; naca-rm-l50d30a; 1953

  370. William J. Nelson and James M. Cubbage, Jr. (Langley Aeronautical Laboratory, Langley Field, Va.); Effects of Slot Size and Geometry on the Flow in Rectangular Tunnels at Mach Numbers up to 1.4; naca-rm-l53b16; 1953

  371. Chester B. Payne (Langley Aeronautical Laboratory, Langley Field, Va.); A Flight Investigation of Some Effects of Automatic Control on Gust Loads; naca-rm-l53e14a; 1953

  372. Delwin R. Croom and Harleth G. Wiley (Langley Aeronautical Laboratory, Langley Field, Va.); Investigation at Transonic Speeds of the Hinge-Moment and Lift-Effectiveness Characteristics of a Single Flap and a Tandem Flap on a 60o Delta Wing; naca-rm-l53e28a; 1953

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