NACA Digital Library - UK Mirror

    136 records

  1. Charles W. Frick, Wallace F. Davis, Lauros M. Randall, Emmet A. Mossman; An Experimental Investigation of NACA Submerged-Duct Entrances; naca-acr-5i20; November, 1945

  2. Herbert S. Ribner; Propellers in yaw; naca-report-820; 1945

  3. Samuel Levey, Kenneth L. Fienup, Ruth M. Wooley; Analysis of square shear web above buckling load; naca-tn-962; February 1945

  4. Shames, Sidney J; Air-consumption parameters for automatic mixture control of aircraft engines; naca-report-804; 1945

  5. Putnam, Abbott A; An analysis of life expectancy of airplane wings in normal cruising flight; naca-report-805; 1945

  6. Benser, William A Moses, Jason J; An investigation of backflow phenomenon in centrifugal compressors; naca-report-806; 1945

  7. Peiser, A M Wilkerson, M; A method of analysis of v-g records from transport operations; naca-report-807; 1945

  8. Brown, Clinton E Parker, Hermon M; A method for the calculation of external lift, moment, and pressure drag of slender open-nose bodies of revolution at supersonic speeds; naca-report-808; 1945

  9. Lundquist, Eugene E Stowell, Elbridge Z Schuette, Evan H; Principles of moment distribution applied to stability of structures composed of bars or plates; naca-report-809; 1945

  10. Mayo, Wilbur L; Analysis and modification of theory for impact of seaplanes on water; naca-report-810; 1945

  11. Male, Donald W Evvard, John C; Preignition-limited performance of several fuels; naca-report-811; 1945

  12. Bellman, Donald R Evvard, John C; Knock-limited performance of several internal coolants; naca-report-812; 1945

  13. Sanders, J C; Correlation of exhaust-valve temperatures with engine operating conditions and valve design; naca-report-813; 1945

  14. Perl, W Tucker, M; A general representation for axial-flow fans and turbines; naca-report-814; 1945

  15. Bullock, Robert O Keetch, Robert C Moses, Jason J; Method of matching performance of compressor systems with that of aircraft power sections; naca-report-815; 1945

  16. Kayten, Gerald G Koven, William; Comparison of wind-tunnel and flight measurements of stability and control characteristics of a Douglas A-26 airplane; naca-report-816; August 11, 1945

  17. Collins, John H Bisson, Edmond E Schmiedlin, Ralph F; Nitrited-steel piston rings for engines of high specific power; naca-report-817; 1945

  18. Manganiello, Eugene J Bogatsky, Donald; An experimental investigation of rectangular exhaust-gas ejectors applicable for engine cooling; naca-report-818; 1945

  19. Ribner, Herbert S; Formulas for propellers in yaw and charts of the side-force derivative; naca-report-819; 1945

  20. Marble, Frank E Ritter, William K Miller, Mahlon A; Effect of NACA injection impeller on mixture distribution of double-row radial aircraft engine; naca-report-821; 1945

  21. Zimmerman, Richard H; Calculations of economy of 18-cylinder radial aircraft engine with exhaust-gas turbine geared to the crankshaft at cruising speed; naca-report-822; 1945

  22. Campbell, John P; Experimental verification of a simplified vee-tail theory and analysis of available data on complete models with vee tails; naca-report-823; 1945

  23. Abbott, Ira H Von Doenhoff, Albert E Stivers, Louis, Jr; Summary of airfoil data; naca-report-824; 1945

  24. Kayten, Gerald G; Analysis of wind-tunnel stability and control tests in terms of flying qualities of full-scale airplanes; naca-report-825; 1945

  25. Cohen, Doris; A method for determining the camber and twist of a surface to support a given distribution of lift, with applications to the load over a sweptback wing; naca-report-826; 1945

  26. Schuette, Evan H; Charts for the minimum-weight design of 24s-t aluminum-alloy flat compression panels with longitudinal z-section stiffeners; naca-report-827; 1945

  27. Sweberg, Harold H Dingeldein, Richard C; Summary of measurements in Langley full-scale tunnel of maximum lift coefficients and stalling characteristics of airplanes; naca-report-829; 1945

  28. Hardy, J K; An analysis of the dissipation of heat in conditions of icing from a section of the wing of the C-46 airplane; naca-report-831; 1945

  29. Graham, Donald J Nitzberg, Gerald E Olson, Robert N; A systematic investigation of pressure distributions at high speeds over five representative NACA low-drag and conventional airfoil sections; naca-report-832; 1945

  30. Allen, H Julian; General theory of airfoil sections having arbitrary shape or pressure distribution; naca-report-833; 1945

  31. Kittel, J Howard; Table of interplanar spacings for crystal-structure determinations by X-ray diffraction with molybdenum, copper, cobalt, iron, and chromium radiations; naca-tn-1000; October 1945

  32. Mayo, Wilbur L; Analysis and modification of theory for impact of seaplanes on water; naca-tn-1008; December 1945

  33. Hoff, N J (Polytechnic Institute of Brooklyn, Brooklyn, N.Y) Boley, Bruno A (Polytechnic Institute of Brooklyn, Brooklyn, N.Y) Klein, Bertram (Polytechnic Institute of Brooklyn, Brooklyn, N.Y); Stresses in and general instability of monocoque cylinders with cutouts II : calculation of the stresses in a cylinder with a symmetric cutout; naca-tn-1014; July 1945

  34. White, Roland J (Curtiss-Wright Corporation) Klampe, Dean G (Curtiss-Wright Corporation); Force and moment coefficients for a thin airfoil with flap and tab in a form useful for stability and control calculations; naca-tn-960; 1945

  35. Mebs, R W (National Bureau of Standards) Mcadam, D J (National Bureau of Standards); Shear elastic properties of some high strength nonferrous metals as affected by plastic deformation and by heat treatment; naca-tn-967; 1945

  36. Hoff, N J (Polytechnic Institute of Brooklyn, Brooklyn, N.Y) Klein, Bertram (Polytechnic Institute of Brooklyn, Brooklyn, N.Y); The inward bulge type buckling of monocoque cylinders III : revised theory which considers the shear strain energy; naca-tn-968; 1945

  37. Bergman, Stefan (Brown University, Providence, R.I); Graphical and analytical methods for the determination of a flow of a compressible fluid around an obstacle; naca-tn-973; 1945

  38. Campbell, William R (National Bureau of Standards); Performance tests of wire strain gages II : calibration factors in compression; naca-tn-978; September 1945

  39. Bennett, J A (National Bureau of Standards); Effect of fatigue-stressing short of failure on some typical aircraft metals; naca-tn-992; October 1945

  40. Leary, J R (Aluminum Company of America) Holt, Marshall (Aluminum Company of America); Column strength of extruded magnesium alloys AM-C58S and AM-C58S-T5; naca-tn-994; December 1945

  41. Jessup, R S (National Bureau of Standards) Cragoe, C S (National Bureau of Standards); Net heat of combustion of AN-F-28 aviation gasolines; naca-tn-996; May 14, 1945

  42. Campbell, William R (National Bureau of Standards); Performance tests of wire strain gages III : calibrations at high tensile strains; naca-tn-997; December 1945

  43. Reid, Elliot G (Stanford, University); Studies of blade shank and pitch distribution for constant-speed propellers; naca-tn-947; 1945

  44. Bruhn, Elmer F (Purdue University); Tests on thin-walled celluloid cylinders to determine the interaction curves under combined bending, torsion, and compression or tension loads; naca-tn-951; 1945

  45. Sechler, E E (California Institute of Technology) Frederick, J L (California Institute of Technology); The strength of semielliptical cylinders subjected to combined loadings; naca-tn-957; February 1945

  46. Keenan, Joseph H (Massachusetts Institute of Technology) Neumann, Ernest P (Massachusetts Institute of Technology); Friction in pipes at supersonic and subsonic velocities; naca-tn-963; 1945

  47. Axilrod, B M (National Bureau of Standards) Jirauch, D H (National Bureau of Standards); Bonding strengths of adhesives at normal and low temperatures; naca-tn-964; 1945

  48. Templin, R L (Aluminum Company of America) Hartmann, E C (Aluminum Company of America); The elastic constants for wrought aluminum alloys; naca-tn-966; 1945

  49. Bers, Lipman (Brown University, Providence, R.I); On a method of constructing two-dimensional subsonic compressible flows around closed profiles; naca-tn-969; 1945

  50. Bers, Lipman (Brown University, Providence, R.I); On the circulatory subsonic flow of a compressible fluid past a circular cylinder; naca-tn-970; 1945

  51. Andrews, H J (Aluminum Company of America) Holt, M (Aluminum Company of America); Fatigue tests on 1/8-inch aluminum alloy rivets; naca-tn-971; February 1945

  52. Bergman, Stefan (Brown University, Providence, R.I); On two-dimensional flows of compressible fluids; naca-tn-972; 1945

  53. Wescoat, C (Aluminum Company of America) Moore, R L (Aluminum Company of America); Bearing strengths of 75S-T aluminum-alloy sheet and extruded angle; naca-tn-974; February 1945

  54. Hamermesh, Bernard (New York University) Reines, Frederick (New York University) Korff, Serge A (New York University); A photoelectric hygrometer; naca-tn-980; May 1945

  55. Moore, R L (Aluminum Company of America) Wescoat, C (Aluminum Company of America); Bearing strengths of 24S-T aluminum alloy plate; naca-tn-981; June 1945

  56. Gwathmey, A T (University of Virginia) Leidheiser, H (University of Virginia) Smith, G P (University of Virginia); The chemical action of oils on single crystals of metals; naca-tn-982; November 1945

  57. Brueggeman, W C (National Bureau of Standards) Mayer, M , Jr (National Bureau of Standards) Smith, W H (National Bureau of Standards); Axial fatigue test at two stress amplitudes of 0.032-inch 24S-T sheet specimens with a circular hole; naca-tn-983; July 1945

  58. Mcadams, William H (Massachusetts Institute of Technology) Nicolai, Lloyd A (Massachusetts Institute of Technology) Keenan, Joseph H (Massachusetts Institute of Technology.); Measurements of recovery factors and coefficients of heat transfer in a tube for subsonic flow of air; naca-tn-985; June 1945

  59. Sachs, George (Case School of Applied Science) Smith, Charles S (Case School of Applied Science) Lubahn, Jack D (Case School of Applied Science) Davis, Gordon E (Case School of Applied Science) Ebert, Lynn J (Case School of Applied Science); Nondestructive measurement of residual and enforced stresses by means of x-ray diffraction I : correlated abstract of the literature; naca-tn-986; September 1945

  60. Sachs, George (Case School of Applied Science) Smith, Charles S (Case School of Applied Science) Lubahn, Jack D (Case School of Applied Science) Davis, Gordon E (Case School of Applied Science) Ebert, Lynn J (Case School of Applied Science); Nondestructive measurement of residual and enforced stresses by means of x-ray diffraction II : some applications to aircraft problems; naca-tn-987; November 1945

  61. Ramberg, Walter (National Bureau of Standards) Mcpherson, A E (National Bureau of Standards) Levy, Samuel (National Bureau of Standards); Strength of wing beams under axial and transverse loads; naca-tn-988; September 1945

  62. Rinker, R C (National Bureau of Standards) Kline, G M (National Bureau of Standards); Survey of adhesives and adhesion; naca-tn-989; August 1945

  63. Weske, John R (Case School of Applied Science); Measurement of the arithmetic mean velocity of a pulsating flow of high velocity by the hot-wire method; naca-tn-990; April 1945

  64. Axilrod, Benjamin M (National Bureau of Standards) Koenig, Evelyn (National Bureau of Standards); Properties of some expanded plastics and other low-density materials; naca-tn-991; September 1945

  65. Pian, Theodore Hsueh-Huang (Massachusetts Institute of Technology); Analytical study of transmission of load from skin to stiffeners and rings of pressurized cabin structure; naca-tn-993; October 1945

  66. Kempner, Joseph; Application of a numerical procedure to stress analysis of stringer-reinforced panels; naca-wr-l-11; March 1945

  67. Joyner, Upshur T; Charts of pressure, density, and temperature changes at an abrupt increase in cross-sectional area of flow of compressible air; naca-wr-l-13; 1945

  68. Bennett, Charles V; Stability and control characteristics of a fighter airplane in inverted flight attitude as determined by model tests; naca-wr-l-15; August 1945

  69. Erwin, Mary A; Hinge moments of sealed-internal-balance arrangements for control surfaces I : theoretical investigation; naca-wr-l-174; August 1945

  70. Church, Oleta; Wind-tunnel investigation of control-surface characteristics XXI : medium and large aerodynamic balances of two nose shapes and a plain overhang used with a 0.40-airfoil-chord flap on an NACA 0009 airfoil; naca-wr-l-175; March 1945

  71. Kenimer, Robert L; An infrared cloud indicator I : analysis of infrared-radiation exchange with tables and chart for calibration of the cloud indicator; naca-wr-l-18; November 1945

  72. Sweberg, Harold H; Note on compressibility effects on downwash at the tail at subcritical speeds; naca-wr-l-19; March 1945

  73. Brilmyer, Harold G; Stresses near the juncture of a closed and an open torsion box as influenced by bulkhead flexibility; naca-wr-l-2; August 1945

  74. Roy, J Albert; Column and plate compressive strengths of aircraft structural materials : 17S-T aluminum-alloy sheet; naca-wr-l-20; June 1945

  75. Kamm, Robert W; Spin-tunnel tests of airplane models with extreme variations in mass distribution along the three body axes; naca-wr-l-22; March 1945

  76. Lietzke, A F; Effect of fuel volatility and mixture temperature on the knocking characteristics of a liquid-cooled single-cylinder test engine; naca-wr-l-26; April 1945

  77. Boyet, H; A method for determining oil-cooler performance requirements in series operation; naca-wr-l-3; September 1945

  78. Roy, J Albert; Column and plate compressive strengths of aircraft structural materials : extruded 24S-T aluminum alloy; naca-wr-l-32; July 1945

  79. Schade, Robert O; Tests of a linked differential flap system designed to minimize the reduction in effective dihedral caused by power; naca-wr-l-4; August 1945

  80. Mourhess, Mary J; Numerical evaluation of the wake-survey equations for subsonic flow including the effect of energy addition; naca-wr-l-5; November 1945

  81. Pendley, Robert E; Effect of propeller-axis angle of attack on thrust distribution over the propeller disk in relation to wake-survey measurement of thrust; naca-wr-l-517; December 1945

  82. Boxer, Emanuel; Wind-tunnel investigation of alternative propellers operating behind deflected wing flaps for the XB-36 airplane; naca-wr-l-533; December 1945

  83. Schultz, Wayne F; Performance selection charts for gliders and twin-engine tow planes; naca-wr-l-537; May 1945

  84. Feigenbaum, D; Estimation of the performance and longitudinal stability and control of a lifting-body type of cargo airplane from tests of simplified models; naca-wr-l-541; June 1945

  85. Migotsky, Eugene; Full-scale-tunnel performance tests of the PV-2 helicopter rotor; naca-wr-l-545; April 1945

  86. Hollingworth, Thomas A; Investigation of effect of sideslip on lateral stability characteristics II : rectangular midwing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface; naca-wr-l-8; April 1945

  87. Luecker, Arthur R; Comparisons of methods of computing bending moments in helicopter rotor blades in the plane of flapping; naca-wr-l-9; August 1945

  88. Galvin, Herman B; Laboratory investigation of icing in the carburetor and supercharger inlet elbow of an aircraft engine I : description of setup and testing technique; naca-wr-e-170; December 1945

  89. Mulholland, Donald R; Laboratory investigation of icing in the carburetor and supercharger inlet elbow of an aircraft engine II : determination of the limiting-icing conditions; naca-wr-e-171; December 1945

  90. Renner, Clark E; Laboratory investigation of icing in the carburetor and supercharger inlet elbow of an aircraft engine V : effect of injection of water-fuel mixtures and water-ethanol-fuel mixtures on the icing characteristics; naca-wr-e-174; December 1945

  91. Brightwell, Virginia L; Relation between fuel economy and crank angle for the maximum rate of pressure rise; naca-wr-e-179; May 1945

  92. Male, Donald W; The effect of six aromatic amines on the preignition-limited performance of 28-R aviation fuel in a CFR engine; naca-wr-e-180; May 1945

  93. Rowe, William H; Process of lead-deposit accumulations on aircraft-engine spark plugs; naca-wr-e-181; December 1945

  94. Kramer, Walter E; Reduction of fuel-vapor loss by omitting some of the fuel constituents normally lost during flight; naca-wr-e-184; August 1945

  95. Kemp, Richard H; Operating stresses in aircraft-engine crankshafts and connecting rods I : slip-ring and bush combinations for dynamic-strain measurements; naca-wr-e-187; May 1945

  96. Cook, Harvey A Held, Louis F Pritchard, Ernest I; The influence of exhaust pressure on knock-limited performance; naca-wr-e-188; April 1945

  97. Brown, Kenneth D; The effect of valve clearance on knock-limited performance and engine cooling; naca-wr-e-189; April 1945

  98. Barnett, Henry C; Smoking characteristics of various fuels as determined by open-cup and laboratory-burner smoke tests; naca-wr-e-190; September 1945

  99. Calvert, Howard F; Operating stresses in aircraft-engine crankshafts and connecting rods II : instrumentation and test results; naca-wr-e-191; August 1945

  100. Addie, A N; Characteristics of the BMW 801D2 automatic engine control as determined from bench tests; naca-wr-e-192; April 1945

  101. Lietzke, A F; Effect of engine-operating variables and internal coolants on spark-advance requirements of a liquid-cooled cylinder; naca-wr-e-198; May 1945

  102. Huppert, Merle C; Nitrous oxide supercharging of an aircraft-engine cylinder; naca-wr-e-199; June 1945

  103. Miller, George R; Control of cylinder temperatures by thermostatically operated internal-coolant valves; naca-wr-e-200; July 1945

  104. Black, Fred O , Jr; A cooling correlation equation for a double-row radial engine based on the temperature of the exhaust-valve seat; naca-wr-e-201; April 1945

  105. Henneberry, Hugh M; Economy of internally cooling only the overheated cylinders of aircraft engines; naca-wr-e-202; July 1945

  106. Tower, Leonard K; Suitability of ethers as aviation fuel components the knock-limited performance of several ethers blended with AN-F-28 fuel; naca-wr-e-207; 1945

  107. Evvard, John C; A relation between knock-limited or preignition-limited air-fuel ratio at lean mixtures and fuel-air ratio at rich mixtures; naca-wr-e-208; November 1945

  108. Calvin C. Blackman and H. Jack White; Flight and Test-Stand Investigation of High-Performance Fuels in Modified Double-Row Radial Air-Cooled Engines III - Knock-Limited Performance of 33-R as Compared With a Triptane Blend and 28-R in Flight; naca-wr-e-263; August 1945

  109. Heinicke, Orville H; Effect of water-alcohol injection and maximum economy spark advance on knock-limited performance and fuel economy of a large air-cooled cylinder; naca-wr-e-264; August 1945

  110. Wilcox, E C; Tests of an adjustable-area exhaust nozzle for jet-propulsion engines; naca-wr-e-265; August 1945

  111. Mesrobian, John M; Air-flow and performance characteristics of the engine-stage supercharger of a double-row radial aircraft engine I : effect of operating variables; naca-wr-e-266; August 1945

  112. Rodgers, Franklin A; The effect of high-resistance ignition cable on the erosion of spark-plug electrodes; naca-wr-e-267; September 1945

  113. Erwin, Robert D , Jr; Effect of maximum cruise-power operation at ultra-lean mixture and increased spark advance on the mechanical condition of cylinder components; naca-wr-e-268; September 1945

  114. Essig, Robert H; Sea-level performance tests of a 22-inch-diameter pulse-jet engine at various simulated ram pressures; naca-wr-e-269; October 1945

  115. Green, L J; The two-dimensional incompressible potential flow over corrugated and distorted infinite surfaces; naca-wr-e-38; 1945

  116. Peters, M D; The effect of high temperature of the cylinder head on the knocking tendency of an air-cooled engine cylinder; naca-wr-e-39; February 1945

  117. Breisch, John H; Endurance tests of a 22-inch-diameter pulse-jet engine with a neoprene-coated valve grid; naca-wr-e-270; October 1945

  118. (Author(s) Not Available); NACA investigation of fuels corresponding to specification AN-F-58 : results of studies in single combustors of J-33, J-34, J-35, and NENE turbojet engines; naca-rm-e8k12; November 16, 1945

  119. Loitsianskii, L. G.; Some basic laws of isotropic turbulent flow; naca-tm-1079; 1945

  120. Ris, V. F.; On the automatic regulation of output in centrifugal compressors; naca-tm-1081; 1945

  121. Mckinney, Elizabeth G; Wind-tunnel investigation of control-surface characteristics XXII : medium and large aerodynamic balances of two nose shapes and a plain overhang used with a 0.20-airfoil-chord flap on an NACA 0009 airfoil; naca-wr-l-196; June 1945

  122. Crane, Robert M.; Computation of hinge-moment characteristics of horizontal tails from section data; naca-wr-a-11; 1945

  123. White, Maurice D.; Estimation of stick-fixed neutral points of airplanes; naca-wr-l-116; 1945

  124. Spearman, M. Leroy.; Wind tunnel investigation of control-surface characteristics XXIII : a 0.25-airfoil-chord flap with tab having a chord twice the flap chord on an NACA 0009 airfoil; naca-wr-l-47; 1945

  125. Fischel, Jack.; Hinge moments of sealed-internal-balance arrangements for control surfaces II : experimental investigation of fabric seals in the presence of a thin-plate overhang; naca-wr-l-52; 1945

  126. Bielat, Ralph P.; A simple method for estimating terminal velocity including effect of compressibility on drag; naca-wr-l-78; 1945

  127. Kelly, Richard L; The low-temperature solubility of 42 aromatic amines in aviation gasoline; naca-wr-e-167; 1945

  128. Lyons, Richard E, Coles, Willard D; Laboratory investigation of icing in the carburetor and supercharger inlet elbow of an aircraft engine III : heated air as a means of de-icing the carburetor and supercharger inlet elbow; naca-wr-e-172; 1945

  129. Shames, Sidney J, Howes, William; Determination of air-consumption parameters for two radial aircraft engines; naca-wr-e-193; 1945

  130. Brown, Kenneth D, Richard, Paul H, Wilson, Robert W; Correlation of the characteristics of single-cylinder and flight engines in tests of high-performance fuels in an air-cooled engine II : knock-limited charge-air flow and cylinder temperatures; naca-wr-e-272; 1945

  131. Hall, Eldon W; A theoretical analysis of the performance of a diesel engine-compressor-turbine combination for aircraft; naca-wr-e-31; 1945

  132. Hollingworth, Thomas A; Investigation of effect of sideslip on lateral stability characteristics III : rectangular low wing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface; naca-wr-l-17; 1945

  133. Bird, J D; Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil; naca-wr-l-172; 1945

  134. Cleary, Harold E; Effects of compressibility on maximum lift coefficients for six propeller airfoils; naca-wr-l-514; 1945

  135. MacDougall, George F, Jr., Scheiter, Leslie E; Longitudinal-trim tests of a 0.059-scale model of the Curtiss-Wright XP-55 airplane; naca-wr-l-538; 1945

  136. Stowell, Elbridge Z, Schwartz, Edward B, Houbolt, John C; Bending and shear stresses developed by the instantaneous arrest of the root of a cantilever beam rotating with constant angular velocity about a transverse axis through the root; naca-wr-l-27; 1945

Last Updated: December 9, 2006, 12:07 pm
Administrator: Paul A S Needham