NACA UK Archive results page

NACA Digital Library - UK Mirror

266 records

Robert G. Deissler; Analysis of turbulent heat transfer, mass transfer, and friction in smooth tubes at high Prandtl and Schmidt numbers; naca-report-1210; 1955
E. R. G. Eckert, A. J. Diaguila; Experimental investigation of free-convection heat transfer in vertical tube at large Grashof numbers; naca-report-1211; 1955
George J. Pack, W. E. Phillips, Jr.; Analog study of interacting and noninteracting multiple-loop control systems for turbojet engines; naca-report-1212; 1955
Hermon M. Parker; Minimum-drag ducted and pointed bodies of revolution based on linearized supersonic theory; naca-report-1213; 1955
Norman S. Silsby; Statistical measurements of contact conditions of 478 transport-airplane landings during routine daytime operations; naca-report-1214; 1955
R. J. Brun, W. Lewis, P. L. Perkins, J. S. Serafin; Impingement of cloud droplets on a cylinder and procedure for measuring liquid-water content and droplet sizes in supercooled clouds by rotating multicylinder method; naca-report-1215; 1955
Kenneth B. Amer, Alfred Gessow; Charts for estimating tail-rotor contribution to helicopter directional stability and control in low-speed flight; naca-report-1216; 1955
John R. Spreiter, Alberta Alksne; Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds; naca-report-1217; 1955
G. Chester Furlong, Thomas V. Bollech; Effect of ground interference on the aerodynamic and flow characteristics of a 42 degree sweptback wing at Reynolds numbers up to 6.8 x 10(6); naca-report-1218; 1955
Wilber B. Huston, T. H. Skopinski; Measurement and analysis of wing and tail buffeting loads on a fighter airplane; naca-report-1219; 1955
E. R. G. Eckert, J. N. B. Livingood; Calculations of laminar heat transfer around cylinders of arbitrary cross section and transpiration-cooled walls with application to turbine blade cooling; naca-report-1220; 1955
Clarence W. Matthews; Theoretical study of the tunnel-boundary lift interference due to slotted walls in the presence of the trailing-vortex system of a lifting model; naca-report-1221; 1955
Alvin Seiff; A free-flight wind tunnel for aerodynamic testing at hypersonic speeds; naca-report-1222; 1955
A. F. Lietzke; Theoretical and experimental investigation of heat transfer by laminar natural convection between parallel plates; naca-report-1223; 1955
Alex Goodman, David T. Thomas, Jr.; Effects of wing position and fuselage size on the low-speed static rolling stability characteristics of a delta-wing model; naca-report-1224; 1955
James J. Donegan, Samuel W. Robinson, Jr., Ordway B. Gates, Jr.; Determination of lateral-stability derivatives and transfer-function coefficients from frequency-response data for lateral motions; naca-report-1225; 1955
Warren A. Tucker; A method for the design of sweptback wings warped to produce specified flight characteristics at supersonic speeds; naca-report-1226; 1955
James J. Gallagher, James N. Mueller; An investigation of the maximum lift of wings at supersonic speeds; naca-report-1227; 1955
Franklin W. Diederich, Martin Zlotnick; Calculated spanwise lift distributions, influence functions, and influence coefficients for unswept wings in subsonic flow; naca-report-1228; 1955
Patrick L. Donoughe, John N. B. Livingood; Exact solutions of laminar-boundary-layer equations with constant property values for porous wall with variable temperaturE; naca-report-1229; 1955
Harvard Lomax, Franklyn B. Fuller, Loma Sluder; Generalized indical forces on deforming rectangular wings in supersonic flight; naca-report-1230; 1955
Ray H. Wright, Vernon G. Ward; NACA transonic wind-tunnel test sections; naca-report-1231; 1955
Kenneth L. Wadlin, Charles L. Shuford, Jr., John McGehee; A theoretical and experimental investigation of the lift and drag characteristics of hydrofoils at subcritical and supercritical speeds; naca-report-1232; 1955
H. S. Ribner; Shock-turbulence interaction and the generation of noise; naca-report-1233; 1955
Charles E. Watkins, Harry L. Runyan, Donald S. Woolston; On the Kernel function of the integral equation relating the lift and downwash distributions of oscillating finite wings in subsonic flow; naca-report-1234; 1955
; Standard atmosphere - tables and data for altitudes to 65,800 feet; naca-report-1235; 1955
Morris D. Friedman, Doris Cohn; Arrangement of fusiform bodies to reduce the wave drag at supersonic speeds; naca-report-1236; 1955
Seth B. Anderson, Richard S. Bray; A flight evaluation of the longitudinal stability characteristics associated with the pitch-up of a swept-wing airplane in maneuvering flight at transonic speeds; naca-report-1237; 1955
Eugene S. Love; Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles; naca-report-1238; 1955
Thomas C. O'Bryan, Edward C. B. Danforth, J. Ford Johnston; Error in airspeed measurement due to the static-pressure field ahead of an airplane at transonic speeds; naca-report-1239; 1955
K. R. Czarnecki, Archibald R. Sinclair; An 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-report-1240; 1955
Howard J. Curfman, Jr.; Theoretical and analog studies of the effects of nonlinear stability derivatives on the longitudinal motions of an aircraft in response to step control deflections and to the influence of proportional automatic control; naca-report-1241; 1955
George E. Solomon; Transonic flow past cone cylinders; naca-report-1242; 1955
George C. Towe, Henry J. Gomberg, J. W. Freemen; High-resolution autoradiography; naca-report-1243; 1955
Stanley Corrsin, Alan L. Kistler; Free-stream boundaries of turbulent flows; naca-report-1244; 1955
Morris Morduchow; Analysis and calculation by integral methods of laminar compressible boundary-layer with heat transfer and with and without pressure gradient; naca-report-1245; 1955
Kenneth L. Wadlin, John A. Ramsen, Victor L. Vaughn, Jr.; The hydrodynamic characteristics of modified rectangular flat plates having aspect ratios of 1.00, 0.25, and 0.125 and operating near a free water surface; naca-report-1246; 1955
P. S. Klebanoff; Characteristics of turbulence in boundary layer with zero pressure gradient; naca-report-1247; 1955
Benjamin Milwitzky, Dean C. Lindquist, Dexter M. Potter; An experimental study of applied ground loads in landing; naca-report-1248; 1955
A. J. Eggers, Jr., Raymond C. Savin; A unified two-dimensional approach to the calculation of three-dimensional hypersonic flows, with application to bodies of revolution; naca-report-1249; 1955
William C. Triplett, Stuart C. Brown, G. Allan Smith; The dynamic-response characteristics of a 35 degree swept-wing airplane as determined from flight measurements; naca-report-1250; 1955
Harvey G. McComb, Jr.; Stress analysis of circular semimonocoque cylinders with cutouts; naca-report-1251; 1955
Jack N. Nielsen; Quasi-cylindrical theory of wing-body interference at supersonic speeds and comparison with experiment; naca-report-1252; 1955
John B. McDevitt; A correlation by means of transonic similarity rules of experimentally determined characteristics of a series of symmetrical and cambered wings of rectangular plan form; naca-report-1253; 1955
Jack D. Brewer; Description and bibliography of NACA research on wing controls - January 1946 - February 1955; naca-rm-54k24; Mar 1955
Joseph W. Semonian, James P. Peterson; An analysis of the stability and ultimate compressive strength of short sheet-stringer panels with special reference to the influence of the riveted connection between sheet and stringer; naca-report-1255; Jan 1955
Ivan E. Beckwith, John A. Moore; An accurate and rapid method for the design of supersonic nozzles; naca-tn-3322; Feb 1955
Allen R. Vick, Paul E. Dewey; An investigation of the discharge and drag characteristics of auxiliary-air outlets discharging into a transonic stream; naca-tn-3466; Jul 1955
Paul E. Dewey; A preliminary investigation of aerodynamic characteristics of small inclined air outlets at transonic Mach numbers; naca-tn-3442; May 1955
William H. Sterbentz, John C. Evvard; Criterions for prediction and control of ram-jet flow pulsations; naca-tn-3506; Aug 1955
Virgil A. Sandborn; Study of the momentum distribution of turbulent boundary layers in adverse pressure gradients; naca-tn-3264; Jan 1955
Virgil A. Sandborn; Experimental evaluation of momentum terms in turbulent pipe flow; naca-tn-3266; Jan 1955
Harold W. Woolley; Effect of dissociation on thermodynamic properties of pure diatomic gases; naca-tn-3270; Apr 1955
M. Metzger, J. Intrater; Intergranular corrosion of high-purity aluminum in hydrochloric acid II : grain-boundary segregation of impurity atoms; naca-tn-3282; Apr 1955
F. S. Sherman; A low-density wind-tunnel study of shock-wave structure and relaxation phenomena in gases; naca-tn-3298; Jul 1955
H. J. Cunningham, R. R. Lundstrom; Description and analysis of a rocket-vehicle experiment on flutter involving wing deformation and body motions; naca-tn-3311; Jan 1955
William M. Bland, Jr., Carl A. Sandhal; A technique utilizing rocket-propelled test vehicles for the measurement of the damping in roll of sting-mounted models and some initial results for delta and unswept tapered wings; naca-tn-3314; May 1955
John DeYoung, Walter H. Barling, Jr.; Prediction of downwash behind swept-wing airplanes at subsonic speed; naca-tn-3346; Jan 1955
Raymond C. Savin; Application of the generalized shock-expansion method to inclined bodies of revolution traveling at high supersonic airspeeds; naca-tn-3349; Apr 1955
A. C. Charters; The linearized equations of motion underlying the dynamic stability of aircraft, spinning projectiles, and symmetrical missiles; naca-tn-3350; Jan 1955
R. D. Johnson, A. P. Young, A. D. Schwope; Plastic deformation of aluminum single crystals at elevated temperatures; naca-tn-3351; Apr 1955
G. B. Dubois, F. W. Ocvirk, R. L. Wehe; Experimental investigation of misaligning couples and eccentricity at ends of misaligned plain bearings; naca-tn-3352; Feb 1955
James R. Reese, John L. Sewall; Effective moment of inertia of fluid in offset, inclined, and swept-wing tanks undergoing pitching oscillations; naca-tn-3353; Jan 1955
James P. Trant, Jr.; Preliminary investigation of a stick shaker as a lift-margin indicator; naca-tn-3355; Feb 1955
J. Mayers, Bernard Budiansky; Analysis of behavior of simply supported flat plates compressed beyond the buckling load into the plastic range; naca-tn-3368; Feb 1955
Conrad Rennemann, Jr.; Minimum-drag bodies of revolution in a nonuniform supersonic flow field; naca-tn-3369; Feb 1955
John M. Hedgepeth, Paul G. Waner, Jr., Robert J. Kell; A simplified method for calculating aeroelastic effects on the roll of aircraft; naca-tn-3370; Mar 1955
Robert F. Peck; Flight measurements of base pressure on bodies of revolution with and without simulated rocket chambers; naca-tn-3372; Apr 1955
Kenneth Margolis; Theoretical calculations of the pressures, forces, and moments due to various lateral motions acting on thin isolated vertical tails with supersonic leading and trailing edges; naca-tn-3373; Mar 1955
Maurice J. Brevoort, Bernard Rashis; Turbulent-heat-transfer measurements at a Mach number of 2.06; naca-tn-3374; Mar 1955
Robert L. Trimpi, Nathaniel B. Cohen; A theory for predicting the flow of real gases in shock tubes with experimental verification; naca-tn-3375; Mar 1955
James H. Walls; An experimental study of orifice coefficients, internal strut pressures, and loads on a small oleo-pneumatic shock strut; naca-tn-3426; Apr 1955
Keith C. Harder, Conrad Rennemann, Jr.; On boattail bodies revolution having minimum wave drag; naca-tn-3478; Aug 1955
William S. Aiken, Bernard Wiener; Analysis of the horizontal-tail loads measured in flight on a multiengine jet bomber; naca-tn-3479; Sep 1955
James J. Kramer, John D. Stanitz; Prediction of losses induced by angle of attack in cascades of sharp-nosed blades for incompressible and subsonic compressible flow; naca-tn-3149; Jan 1955
Kaattari, George E; Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 2.46 and 3.36; naca-rm-a54j12; January 18, 1955
Eggers, A J , Jr Hermach, C A; Initial experiments on the aerodynamic cooling associated with large-scale vortical motions in supersonic flow; naca-rm-a54l13; March 08, 1955
Mellenthin, Jack A; The effect of a 4-percent-high spoiler on buffeting forces on a naca 65(sub 06)A004 two-dimensional airfoil at subsonic Mach numbers; naca-rm-a54l22; March 23, 1955
Bright, Loren G; A flight investigation at transonic speeds of a model having a triangular wing of aspect ratio 4; naca-rm-a54l27; March 24, 1955
Hunton, Lynn W; A study of the application of airfoil section data to the estimation of the high-subsonic-speed characteristics of swept wings; naca-rm-a55c23; June 24, 1955
Delany, Noel K; Exploratory investigation of the low-speed static stability of a configuration employing three identical triangular wing panels and a body of equal length; naca-rm-a55c28; April 29, 1955
Dugan, Duane W; Experimental investigation of some aerodynamic effects of a gap between wing and body of a moderately slender wing-body combination at a Mach number of 1.4; naca-rm-a55d08; May 27, 1955
Kaattari, George E Hill, William A , Jr Nielsen, Jack N; Controls for supersonic missiles; naca-rm-a55d12; May 27, 1955
Triplett, William C; Considerations involved in the design of a roll-angle computer for a bank-to-turn interceptor; naca-rm-a55d18a; June 1955
Eggers, A J , Jr Hansen, Frederick Cunningham, Bernard E; Theoretical and experimental investigation of the effect of yaw on heat transfer to circular cylinders in hypersonic flow; naca-rm-a55e02; July 25, 1955
Katzen, Elliott D Pitts, William C; Load distributions on wings and wing-body combinations at high angles of attack and supersonic speeds; naca-rm-a55e17; July 21, 1955
Seiff, Alvin Allen, H Julian; Some aspects of the design of hypersonic boost-glide aircraft; naca-rm-a55e26; August 15, 1955
Jorgensen, Leland H Perkins, Edward W; Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 1.98; naca-rm-a55e31; August 23, 1955
Reese, David E , Jr; An experimental investigation of the unsteady lift induced on a wing in the downwash field of an oscillating canard control surface; naca-rm-a55f01; August 15, 1955
Canning, Thomas N Derose, Charles E; Drag and rolling-moment effectiveness of trailing-edge spoilers at Mach numbers 2.2 and 5.0; naca-rm-a55f15; October 03, 1955
Eggers, A J , Jr; A discussion of methods for reducing aerodynamic heating in supersonic flight; naca-rm-a55f21a; September 1955
Pfyl, Frank A; An investigation of the effects of nose and lip shapes for an underslung scoop inlet at Mach numbers from 0 to 1.9; naca-rm-a55g13; November 18, 1955
Reller, John O Hamaker, Frank M; Temperature recovery factors on a slender 12 degree cone-cylinder at Mach numbers from 3.0 to 6.3 and angles of attack up to 45 degrees; naca-rm-a55g20; October 03, 1955
Dennis, David H Syvertson, Clarence A; Effects of boundary-layer separation on normal force and center of pressure of a cone-cylinder model with a large base flare at Mach numbers from 3.00 to 6.28; naca-rm-a55h09; October 03, 1955
Eggers, A J , Jr; A method for simulating the atmospheric entry of long-range ballistic missiles; naca-rm-a55i15; December 28, 1955
Rubesin, Morris W Pappas, Constantine C Okuno, Arthur F; The effect of fluid injection on the compressible turbulent boundary layer : preliminary tests on transpiration cooling of a flat plate; naca-rm-a55i19; December 21, 1955
Reese, David E JR Carlson, William C A; An experimental investigation of the hinge-moment characteristics of a constant-chord control surface oscillating at high frequency; naca-rm-a55j24; December 1955
Conrad, E William; Preliminary analysis of performance of turbojet engines used as pumps for boundary-layer control; naca-rm-e55e20a; August 16, 1955
Childs, J Howard Friedman, Robert Kochendorfer, Fred D Lubick, Robert J; Stall and flame-out resulting from firing of armament; naca-rm-e55e25; August 05, 1955
Dorsch, Robert G Serafini, John S Fletcher, Edward A; A preliminary investigation of static-pressure changes associated with combustion of aluminum borohydride in a supersonic wind tunnel; naca-rm-e55f07; August 18, 1955
Henzel, James G , Jr Mcardle, Jack G; Preliminary performance data of several tail-pipe-cascade-type model thrust reversers; naca-rm-e55f09; August 29, 1955
Hurrell, Herbert G Vasu, George Dunbar, William R; Experimental study of shock-positioning method of ram-jet-engine control; naca-rm-e55f21; August 29, 1955
Reynolds, T W; Aircraft-fuel-tank design for liquid hydrogen; naca-rm-e55f22; August 09, 1955
Smith, Kenneth J Osborn, Walter M; Design and test of mixed-flow impellers VI : performance and parabolic-bladed impeller with shroud redesigned by rapid approximate method; naca-rm-e55f23; September 07, 1955
Piercy, Thomas G Klann, John L; Experimental investigation of methods of improving diffuser-exit total-pressure profiles for side-inlet model at Mach number 3.05; naca-rm-e55f24; August 29, 1955
Rabb, Leonard Simpkinson, Scott H; Free-flight heat-transfer measurements on two 20 degree-cone-cylinders at Mach numbers from 1.3 to 4.9; naca-rm-e55f27; July 18, 1955
Perkins, Porter J; Statistical survey of icing data measured on scheduled airline flights over the United States and Canada from November 1951 to June 1952; naca-rm-e55f28a; September 08, 1955
Conners, James F Meyer, Rudolph C; Performance characteristics of axisymmetric two-cone and isentropic nose inlets at Mach number 1.90; naca-rm-e55f29; December 07, 1955
Englert, Gerald W Wasserbauer, Joseph F Whalen, Paul; Interaction of a jet and flat plate located in an airstream; naca-rm-e55g19; September 08, 1955
Altschuller, Aubrey P; Calculated heats of formation and combustion of boron compounds (boron, hydrogen, carbon, silicon); naca-rm-e55g26; October 04, 1955
Esgar, Jack B Ziemer, Robert R; Review of status, methods and potentials of gas-turbine air-cooling; naca-rm-e54i23; February 23, 1955
Piercy, Thomas G; Preliminary investigation of some internal boundary-layer-control systems on a side inlet at Mach number 2.96; naca-rm-e54k01; February 18, 1955
Foster, Hampton H Fletcher, Edward A Straight, David M; Aluminum borohydride - hydrocarbon mixtures as a source of ignition for a turbojet combustor; naca-rm-e54k12; February 23, 1955
Morgan, W C Kemp, R H; An experimental evaluation of several design variations of hollow turbine blades for expendable engine application; naca-rm-e54k23; February 23, 1955
Harry, David P , III Lubick, Robert J; Inlet-air distortion effects on stall, surge, and acceleration margin of a turbojet engine equipped with variable compressor inlet guide vanes; naca-rm-e54k26; October 04, 1955
Steffen, Fred W Krull, H George Schmiedlin, Ralph F; Effects of several geometric variables on internal performance of short convergent-divergent exhaust nozzles; naca-rm-e54l09; February 18, 1955
Baughman, L Eugene; Wind-tunnel investigation at Mach 1.9 of multijet-missile base pressures; naca-rm-e54l14; March 1955
Wise, G A Campbell, R C; Investigation of a ramp-type inlet designed for improved angle-of-attack performance at Mach number 2.0; naca-rm-e54l17; February 23, 1955
Wilcox, Fred A Hearth, Donald P; Application of oblique-shock sensing system to ram-jet-engine flight Mach number control; naca-rm-e54l22a; March 03, 1955
Morris, James F Caves, Robert M Lord, Albert M; Blow-out velocities of several slurry and liquid fuels in a 1 7/8 inch-diameter combustor; naca-rm-e54l27a; February 23, 1955
Olson, Walter T Breitwieser, Roland; NACA research on slurry fuels through 1954; naca-rm-e55b14; April 21, 1955
Kerslake, William R Dangle, E E Cervenka, A J; Experimental evaluation of boron-hydrocarbon slurry in a 16-inch ram-jet combustor; naca-rm-e55c07; July 1955
Silverstein, Abe Hall, Eldon W; Liquid hydrogen as a jet fuel for high-altitude aircraft; naca-rm-e55c28a; April 15, 1955
Hearth, Donald P Englert, Gerald W Kowalski, Kenneth L; Matching of auxiliary inlets to secondary-air requirements of aircraft ejector exhaust nozzles; naca-rm-e55d21; August 16, 1955
Hamrick, Joseph T Osborn, Walter M; Design and test of mixed-flow impellers V : design procedure and performance results for two vaned diffusers tested with impeller model MFI-1B; naca-rm-e55e13; July 07, 1955
Chiarito, Patrick T; Effectiveness of a turbojet tubular combustor in screening the turbine from foreign objects; naca-rm-e55e16; July 18, 1955
Kremzier, Emil J Wise, George A; Effect of centerbody boundary-layer removal near the throat of three coniccal nose inlets at Mach 1.6 to 2.0; naca-rm-e55h16a; November 15, 1955
Rabb, Leaonard Disher, John H; Boundary-layer transition at high Reynolds numbers as obtained in flight of a 20 degree cone-cylinder with wall to local stream temperature ratios near 1.0; naca-rm-e55i15; November 03, 1955
Witzke, Walter R Prok, George M Keller, Thomas A; Design considerations of a condensing system for vaporized magnesium; naca-rm-e55i20; November 30, 1955
Ordin, Paul M; Transportation of liquid fluorine; naca-rm-e55i23; November 08, 1955
Allen, John L; Preliminary investigation of effect on performance of dividing conical-spike nose inlets into halves at Mach numbers 1.5 to 2.0; naca-rm-e55i26; December 19, 1955
Pinkel, Benjamin Deutsch, George C Morgan, William C; Preliminary investigation of several root designs for cermet turbine blades in turbojet engine III : curved-root design; naca-rm-e55j04; December 28, 1955
Tomazic, William A; Rocket-engine throttling; naca-rm-e55j20; 1955
Lindsey, Walter F Landrum, Emma Jean; Flow and force characteristics of 2-percent-thick airfoils at transonic speeds; naca-rm-l54i30; January 18, 1955
Peck, Robert F; Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8; naca-rm-l54j29a; January 18, 1955
Welsh, Clement J Wallskog, Harvey A Sandahl, Carl A; Effects of some leading-edge modifications, section and plan-form variations, and vertical position on low-lift wing drag at transonic speeds; naca-rm-l54k01; January 18, 1955
Alford, William J Silvers, H Norman King, Thomas, J , jr; Experimental aerodynamic forces and moments at low speed of a missile model during simulated launching from the midsemispan location of a 45 degree sweptback wing-fuselage combination; naca-rm-l54k11a; February 04, 1955
Parks, James H; Transonic longitudinal aerodynamic effects of sweeping up the rear of the fuselage of a rocket-propelled airplane model having no horizontal tail; naca-rm-l54k12; January 20, 1955
Kuhn, Richard E Byrnes, Andrew L , Jr; Aerodynamic loading characteristics in sideslip of a 45 degree sweptback wing with and without a fence at high subsonic speeds; naca-rm-l54k15; January 28, 1955
Bridgland, T F , Jr; A theoretical investigation of the effect of auxiliary damping on the longitudinal response of a transonic bomber configuration in flight through continuous turbulence; naca-rm-l54k15a; March 1955
English, Roland D; Free-flight investigation, including some effects of wing aeroelasticity, of the rolling effectiveness of an all-movable horizontal tail with differential incidence at Mach numbers from 0.6 to 1.5; naca-rm-l54k30; January 25, 1955
Curfman, Howard J , Jr; Application of nonlinear aerodynamic stability characteristics to simplify missile control and guidance systems; naca-rm-l54l06a; February 15, 1955
Chauvin, Leo T Maloney, Joseph P; Turbulent convective heat-transfer coefficients measured from flight tests of four research models (NACA RM-10) at Mach numbers from 1.0 to 3.6; naca-rm-l54l15; March 11, 1955
Vitale, A James; Characteristics of loads in rough air at transonic speeds of rocket-powered models of a canard and a conventional-tail configuration; naca-rm-l54l17; March 1955
Piland, Robert O; Performance measurements from a rocket-powered exploratory research missile flown to a Mach number of 10.4; naca-rm-l54l29a; March 15, 1955
Fischetti, Thomas L Loving, Donald L; Effect of an all-movable wing-tip control on the longitudinal stability of 60 degree sweptback-wing-indented-body configuration equipped with fences at transonic speeds; naca-rm-l54l30; April 04, 1955
Platt, Robert J , Jr Brooks, Joseph D; Transonic wind-tunnel investigation of the effects of sweepback and thickness ratio on the wing loads of a wing-body combination of aspect ratio 4 and taper ratio 0.6; naca-rm-l54l31b; April 04, 1955
Palmer, William E Burrows, Dale L; A transonic wind-tunnel investigation of the longitudinal force and moment characteristics of two delta wings and one clipped-tip delta wing of 4 percent thickness on a slender body; naca-rm-l55a07a; April 04, 1955
Alford, William J , Jr; Experimental static aerodynamic forces and moments at low speed on a canard missle during simulated launching from the midsemispan and wing-tip locations of a 45 degree sweptback wing-fuselage combination; naca-rm-l55a12; April 06, 1955
Wallskog, Harvey A; Flutter experiences with thin pointed-tip wings during flight tests of rocket-propelled models at Mach numbers from 0.8 to 1.95; naca-rm-l55a14; April 04, 1955
Rumsey, Charles B Piland, Robert O Hopko, Russell N; Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5; naca-rm-l55a14a; March 11, 1955
Ulmann, Edward F Smith, Fred M; Aerodynamic characteristics of a 60 degree delta wing having a half-delta tip control at a Mach number of 4.04; naca-rm-l55a19; April 25, 1955
Bartlett, Walter, A , jr Hagginbotham, William K , Jr; Flight and preflight tests of a ram jet burning magnesium slurry fuel and utilizing a solid-propellant gas generator for fuel expulsion; naca-rm-l55a24; April 06, 1955
Henry, Beverly Z , Jr Cahn, Maurice S; Preliminary results of an investigation at transonic speeds to determine the effects of a heated propulsive jet on the drag characteristics of a related series of afterbodies; naca-rm-l55a24a; March 25, 1955
Bertram, Mitchel H Mccauley, William D; An investigation of the aerodynamic characteristics of thin delta wings with a symmetrical double-wedge section at a Mach number of 6.9; naca-rm-l55b14; October 14, 1955
Spearman, M Leroy; Investigation of the aerodynamic characteristics in pitch and sideslip of a 45 degree sweptback-wing airplane model with various vertical locations of the wing and horizontal tail : effect of wing location and geometric dihedral for the wing-body com; naca-rm-l55b18; April 06, 1955
Thompson, Robert F Taylor, Robert T; Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of an aileron located at two spanwise positions; naca-rm-l55b18a; May 10, 1955
Coletti, Donard E; Investigation of interference lift, drag, and pitching moment of a series of triangular wing and body combinations at a Mach number of 1.62; naca-rm-l55b25; May 27, 1955
Nason, Martin L Rock, Rupert S Brown, Clarence, Jr; An evaluation of a rolleron-roll-rate-stabilization system for a canard missile configuration at Mach numbers from 0.9 to 2.3; naca-rm-l55c22; September 15, 1955
Chauvin, Leo T Carter, Howard S; Exploratory tests of transpiration cooling on a porous 8 degree cone at M = 2.05 using nitrogen gas, helium gas, and water as the coolants; naca-rm-l55c29; June 03, 1955
Dow, Norris F Peters, Roger W; Preliminary investigation of the failure of pressurized stiffened cylinders; naca-rm-l55d15b; May 20, 1955
Alford, William J , Jr Silvers, H Norman King, Thomas J , Jr; Experimental static aerodynamic forces and moments at low speed on a missile model during simulated launching from the 25-percent-semispan and wing-tip location of a 45 degree sweptback wing-fuselage combination; naca-rm-l55d20; May 25, 1955
Wiley, Harleth G Moseley, William C , Jr; An investigation at high subsonic speeds of the effects of horizontal-tail height on the aerodynamic and loading characteristics in sideslip on a 45 degree sweptback, untapered tail assembly as determined from force tests and integrated vertical-tail; naca-rm-l55e04; June 28, 1955
Smith, Norman F Carlson, Harry W; Some effects of configuration variables on store loads at supersonic speeds; naca-rm-l55e05; July 06, 1955
Bressette, Walter E Faget, Maxime A; An investigation of jet effects on adjacent surfaces; naca-rm-l55e06; June 28, 1955
Jones, Jim J; Experimental drag coefficients of round noses with conical windshields at Mach number 2.72; naca-rm-l55e10; June 28, 1955
Davis, Don D , Jr Hieser, Gerald; Loads on thin wings at transonic speeds; naca-rm-l55e11c; June 28, 1955
Czarnecki, K R Lord, Douglas R; Simplified procedures for estimating flap-control loads at supersonic speeds; naca-rm-l55e12; May 27, 1955
Lord, Douglas, R Czarnecki, K R; Loads associated with spoilers at supersonic speeds; naca-rm-l55e12a; June 14, 1955
Runckel, Jack F Gray, W H; An investigation of loads on ailerons at transonic speeds; naca-rm-l55e13; May 27, 1955
Guy, Lawrence D; Loads on external stores at transonic and supersonic speeds; naca-rm-l55e13b; August 15, 1955
Silsby, Norman S Harrin, Eziaslav N; Landing conditions for large airplanes in routine operations; naca-rm-l55e18c; July 06, 1955
Polhamus, Edward C; Some factors affecting the variation of pitching moment with sideslip of aircraft configurations; naca-rm-l55e20b; July 15, 1955
Carlson, Harry W Gapcynski, John P; An experimental investigation at a Mach number of 2.01 of the effects of body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations; naca-rm-l55e23; July 21, 1955
Feller, William V; Investigation of equilibrium temperatures and average laminar heat-transfer coefficients for the front half of swept circular cylinders at a Mach number of 6.9; naca-rm-l55f08a; August 18, 1955
Beckwith, Ivan E; Theoretical investigation of laminar heat transfer on yawed infinite cylinders in supersonic flow and a comparison with experimental data; naca-rm-l55f09; August 09, 1955
Falanga, Ralph A; A free-flight investigation of the effects of simulated sonic turbojet exhaust on the drag of a boattail body with various jet sizes from Mach number 0.87 to 1.50; naca-rm-l55f09a; August 18, 1955
Griffith, George E Miltonberger, Georgene H Rosecrans, Richard; Tests of aerodynamically heated multiweb wing structures in a free jet at Mach number 2 : two aluminum-alloy models of 20-inch chord with 0.064- and 0.081-inch-thick skin; naca-rm-l55f13; August 09, 1955
Strass, H Kurt Stephens, Emily W Fields, E M Schult, Eugene D; Collection and summary of flap-type-aileron rolling-effectiveness data at zero lift as determined by rocket-powered model tests at Mach numbers between 0.6 and 1.6; naca-rm-l55f14; September 02, 1955
Passera, Anthony L Garner, H Douglas; Simulator studies of a simple homing system; naca-rm-l55g06; October 06, 1955
Schult, Eugene D; :A Free-flight investigation at high subsonic and low supersonic speeds of the rolling effectiveness and drag of three spoiler controls having potentially low actuating-force requirements; naca-rm-l55g11a; September 20, 1955
Rumsey, Charles B; Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration; naca-rm-l55g28a; October 07, 1955
Seaberg, Ernest C Sproull, Royce H Reid, H J E , Jr; Flight investigation at supersonic Mach numbers of an automatic acceleration control missile in which rate damping is obtained from a linear accelerometer placed ahead of the missile center of gravity; naca-rm-l55g29; November 08, 1955
Hoffman, Sherwood; Free-flight tests to determine the power-on and power-off pressure distribution and drag of the NACA RM-10 research vehicle at large Reynolds numbers between Mach numbers 0.8 and 3.0; naca-rm-l55h02; September 20, 1955
Guy, Lawrence D Hadaway, William M; Aerodynamic loads on an external store adjacent to a 45 degree sweptback wing at Mach numbers from 0.70 to 1.96, including an evaluation of techniques used; naca-rm-l55h12; November 15, 1955
Turner, Thomas R Vogler, Raymond D; Wind-tunnel investigation at transonic speeds of a jet control on an 80 degree delta-wing missile; naca-rm-l55h22; November 1955
Gapcynski, John P; An experimental investigation of the flow phenomena over bodies at high angles of attack at a Mach number of 2.01; naca-rm-l55h29; October 27, 1955
Clements, James E; A theoretical analysis of a simple aerodynamic device to improve the longitudinal damping of a cruciform missile configuration at supersonic speeds; naca-rm-l55h31; October 27, 1955
Purser, Paul E; Comparative dispersion data from ground-launched 2.25-inch rockets equipped with cruciform and monoplane fins; naca-rm-l55i06; November 1955
Gillespie, Warren, Jr; Lift, drag, and longitudinal stability at Mach numbers from 1.4 to 2.3 of a rocket-powered model having a 52.5 degree sweptback wing of aspect ratio 3 and inline tail surfaces; naca-rm-l55i12; December 15, 1955
Falanga, Ralph A Judd, Joseph H; Flight investigation of the effect of underwing propulsive jets on the lift, drag, and longitudinal stability of a delta-wing configuration at Mach numbers from 1.23 to 1.62; naca-rm-l55i13; December 15, 1955
Coletti, Donald E; Investigation of interference lift, drag, and pitching moment of a series of triangular-wing and body combinations at a Mach number of 1.94; naca-rm-l55i14; December 21, 1955
Schmeer, James W; The effect of leading-edge droop upon the pressure distribution and aerodynamic loading characteristics of a 45 degree sweptback wing at transonic speeds; naca-rm-l55i16; November 08, 1955
Press, Harry Meadows, May T Hadlock, Ivan; Estimates of probability distribution of root-mean-square gust velocity of atmospheric turbulence from operational gust-load data by random-process theory; naca-tn-3362; March 1955
Keith, Arvid L , Jr Schiff, Jack; Low-speed wind-tunnel investigation of a triangular sweptback air inlet in the root of a 45 degree sweptback wing; naca-tn-3363; 1955
Reller, John O , Jr Hamaker, Frank M; An experimental investigation of the base pressure characteristics of nonlifting bodies of revolution at Mach numbers from 2.73 to 4.98; naca-tn-3393; March 17, 1955
Daley, Bernard N Lord, Douglas R; Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 degrees to 20 degrees at high subsonic speeds; naca-tn-3424; May 1955
Bird, John D; Some calculations of the lateral response of two airplanes to atmospheric turbulence with relation to the lateral snaking problem; naca-tn-3425; May 1955
Seaberg, Ernest C; Theoretical investigation of a proportional-plus-flicker automatic pilot; naca-tn-3427; May 1955
Pendley, Robert E Robinson, Harold L; An investigation of several NACA 1-series nose inlets with and without protruding central bodies at high-subsonic Mach numbers and at a Mach number of 1.2; naca-tn-3436; May 1955
Nichols, Mark R Pierpont, Kenneth P; Preliminary investigation of a submerged air scoop utilizing boundary-layer suction to obtain increased pressure recovery; naca-tn-3437; April 1955
Watkins, Charles E Berman, Julian H; On the Kernel function of the integral equation relating lift and downwash distributions of oscillating wings in supersonic flow; naca-tn-3438; May 1955
Mccomb, Harvey G , Jr Low, Emmet F , Jr; Tables of coefficients for the analysis of stresses about cutouts in circular semimonocoque cylinders with flexible rings; naca-tn-3460; July 1955
Turner, Thomas R; Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds; naca-tn-3468; July 1955
Gessow, Alfred Tapscott, Robert J; Supplementary charts for estimating performance of high-performance helicopters; naca-tn-3482; July 1955
Turner, Howard L White, John S Van Dyke, Rudolph D , Jr; Flight testing by radio remote control-flight evaluation of a beep-control system; naca-tn-3496; March 1955
Beck, Preston E (Naval Air Test Center); Some results of flight testing of ski-equipped aircraft at the Naval Air Test Center; naca-rm-54j27; February 04, 1955
(Author(s) Not Available); Meteorological problems associated with commercial turbojet-aircraft operation; naca-rm-54l29; June 21, 1955
Black, John M (Forest Products Laboratory) Blomquist, R F (Forest Products Laboratory); Metal-bonding adhesives for high-temperature service; naca-rm-55f08; July 28, 1955
Cesaro, Richard S Walker, Curtis L; Application of non-afterburning turbojets to supersonic flight; naca-rm-55k16; November 18, 1955
Wetzel, Benton E; Wind-tunnel investigation at subsonic and supersonic speeds of a fighter model employing a low-aspect-ratio unswept wing and a horizontal tail mounted well above the wing plane-lateral and directional stability; naca-rm-a54h26b; April 28, 1955
Eggers, A J , Jr Syverton, Clarence A; Experimental investigation of a body flare for obtaining pitch stability and a body flap for obtaining pitch control in hypersonic flight; naca-rm-a54j13; January 18, 1955
Turner, Howard L Triplett, William C White, John S; A flight and analog computer study of some stabilization and command networks for an automatically controlled interceptor during the final attack phase; naca-rm-a54j14; March 23, 1955
Baldwin, Barrett S , Jr Dickey, Robert R; Application of wing-body theory to drag reduction at low supersonic speeds; naca-rm-a54j19; January 28, 1955
Wetzel, Benton E; Effect of taper ratio on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 with 53.1 degrees sweepback of leading edge at subsonic and supersonic speeds; naca-rm-a54j20; January 27, 1955
Sammonds, Robert I Reynolds, Robert M; The pressure-recovery and propeller-force characteristics of a propeller-spinner-cowling combination employing NACA 4-(5) (05)-037 six- and eight-blade dual-rotation propellers with an NACA 1 series D-type cowl; naca-rm-a54j22; January 27, 1955
Tunnell, Phillips J; An investigation of string support interference on base pressure and forebody chord force at Mach numbers from 0.60 to 1.30; naca-rm-a54k16a; January 28, 1955
Sutton, Fred B Dickson, Jerald K; The longitudinal characteristics at Mach numbers up to 0.92 of several wing-fuselage-tail combinations having sweptback wings with NACA four-digit thickness distributions; naca-rm-a54l08; March 24, 1955
Eggers, Alfred J , Jr Allen, H Julian Neice, Stanford E; A comparative analysis of the performance of long-range hypervelocity vehicles; naca-rm-a54l10; March 24, 1955
Knechtel, Earl D Summers, James L; Effects of sweep and taper on the longitudinal characteristics of an aspect ratio 3 wing-body combination at Mach numbers from 0.6 to 1.4; naca-rm-a55a03; March 23, 1955
Sadoff, Melvin; Summary of the flight conditions and maneuvers in which maximum wing and tail loads were experienced on a swept-wing fighter airplane; naca-rm-a55a06; March 30, 1955
Alksne, Alberta; A comparison of two methods for computing the wave of wing-body combinations; naca-rm-a55a06a; April 07, 1955
Hopkins, Edward J Sorensen, Norman E; Downwash survey behind two low-aspect-ratio variable-incidence wings in combination with three different size fuselages at a Mach number of 0.25; naca-rm-a55a07; March 30, 1955
Mossman, Emmet A Lazzeroni, Frank A Pfyl, Frank A; An experimental investigation of the air-flow of a scoop-type normal-shock inlet; naca-rm-a55a13; April 28, 1955
Lomax, Harvard; The wave drag of arbitrary configurations in linearized flow as determined by areas and forces in oblique planes; naca-rm-a55a18; March 24, 1955
Beam, Benjamin H Reed, Verlin D Lopez, Armando E; Wind-tunnel measurements at subsonic speeds of the static and dynamic-rotary stability derivatives of a triangular-wing airplane model having a triangular vertical tail; naca-rm-a55a28; April 25, 1955
Blackaby, James R; Wind-tunnel investigation at low speed of a wing having 63 degree sweepback and a drooped tip; naca-rm-a55b14; April 07, 1955
Mcdevitt, John B; An experimental investigation of two methods for reducing transonic drag of swept-wing and body combinations; naca-rm-a55b21; April 29, 1955
Polentz, Perry P Page, William A Levy, Lionel L , Jr; The unsteady normal-force characteristics of selected NACA profiles at high subsonic Mach numbers; naca-rm-a55c02; May 27, 1955
Walker, Harold J Maillard, William C; A correlation of airfoil section data with the aerodynamic loads measured on a 45 degree sweptback wing model at subsonic Mach numbers; naca-rm-a55c08; May 27, 1955
Neice, Stanford E Wong, Thomas J Hermach, Charles A; Lift, drag, and static longitudinal stability characteristics of four airplane-like configurations at Mach numbers from 3.00 to 6.28; naca-rm-a55c24; April 25, 1955
Dickson, Jerald K Sutton, Fred B; The effect of wing height on the longitudinal characteristics at high subsonic speeds of a wing-fuselage-tail combination having a wing with 40 degrees of sweepback and NACA four digit thickness distribution; naca-rm-a55c30; May 25, 1955
Dickson, Gerald K Sutton, Fred B; The effect of wing fences on the longitudinal characteristics at Mach numbers up to 0.92 of a wing-fuselage-tail combination having a 40 degree sweptback wing with NACA 64A thickness distribution; naca-rm-a55c30a; May 27, 1955
Graham, David Evans, William T; Investigation of the effects of an airfoil section modification on the aerodynamic characteristics at subsonic and supersonic speeds of a thin swept wing of aspect ratio 3 in combination with a body; naca-rm-a55d11; June 28, 1955
Cole, Henry A , Jr Brown, Stuart C Holleman, Euclid C; The effects of flexibility on the longitudinal and lateral directional response of a large airplane; naca-rm-a55d14; May 27, 1955
White, Maurice D; A flight investigation at transonic speeds of a model having a triangular wing of aspect ratio 3; naca-rm-a55d18; June 24, 1955
Mossman, Emmett A Pfyl, Frank A Lazzeroni, Frank A; Experimental investigation at Mach numbers from 0 to 1.9 of trapezoidal and circular side inlets for a fighter-type airplane; naca-rm-a55d27; July 28, 1955
Stephenson, Jack D Selan, Ralph Bandettini, Angelo; A comparison at Mach numbers up to 0.92 of the calculated and experimental downwash and wake characteristics at various horizontal tail heights behind a wing with 45 degree of sweepback; naca-rm-a55d27a; June 28, 1955
Stewart, Elwood C; Application of statistical theory to beam-rider guidance in the presence of noise I : Wiener filter theory; naca-rm-a55e11; August 23, 1955
Delany, Noel K; Additional measurements of the low-speed static stability of a configuration employing three triangular wing panels and a body of equal length; naca-rm-a55f02a; July 25, 1955
Holdaway, George H; Additional comparisons between computed and measured transonic drag-rise coefficients at zero lift for wing-body-tail configurations; naca-rm-a55f06; August 15, 1955
Cooper, George E Innis, Robert C; Effect of area-suction-type boundary-layer control on the landing-approach characteristics of a 35 degree swept-wing fighter; naca-rm-a55k14; February 03, 1955
Peterson, Victor L Menees, Gene P; Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22 : lateral-directional characteristics of a triangular wing and canard; naca-rm-a57l18; March 28, 1955
Gillespie, Warren, Jr; Lift, drag, and longitudinal stability at Mach numbers from 0.8 to 2.1 of a rocket-powered model having a tapered unswept wing of aspect ratio 3 and inline tail surfaces; naca-rm-l55b10; April 25, 1955
Cubbage, James M , Jr; Effect of convergent ejector nozzles on the boattail drag of a 16 degree conical afterbody at Mach numbers of 0.6 to 1.26; naca-rm-l58g25; September 17, 1955
Keune, Friedrich.; Lift on a bent, flat plate; naca-tm-1340; 1955
Vladimirov, A. N.; Approximate hydrodynamic design of a finite span hydrofoil; naca-tm-1341; 1955
Germain, Paul.; General theory of conical flows and its application to supersonic aerodynamics; naca-tm-1354; 1955
Miele, Angelo.; General solutions of optimum problems in nonstationary flight; naca-tm-1388; 1955
Miele, Angelo.; Optimum flight paths of turbojet aircraft; naca-tm-1389; 1955
Loeb, Julian.; From linear mechanics to nonlinear mechanics; naca-tm-1396; 1955
Rothrock, Addison M.; Turbojet propulsion-system research and the resulting effects on airplane performance; naca-rm-54h23; 1955
Neel, Carr B., Jr.; A Heated-Wire Liquid-Water-Content Instrument and Results of Initial Flight Tests in Icing Conditions; naca-rm-a54i23; 1955
Dods, Jules B. Jr., Tinling, Bruce E.; Summary of results of a wind-tunnel investigation of nine related horizontal tails; naca-tn-3497; 1955
Deyoung, John Barling, Walter H , Jr; Correction of additional span loadings computed by the Weissinger seven-point method for moderately tapered wings of high aspect ratio; naca-tn-3500; July 1955
Sadoff, Melvin., Matteson, Frederick H., Havill, C. Dewey.; A method for evaluating the loads and controllability aspects of the pitch-up problem; naca-rm-a55d06; 1955
Matthews, Howard F., Schmidt, Stanley F.; A comparison of the maneuvering performance of a monowing versus a cruciform missile; naca-rm-a55d13; 1955
Rathert, George A , Jr Abramovitz, Marvin Gadeberg, Burnett L; The effects of powered controls and fire-control systems on tracking accuracy; naca-rm-a55d12a; May 26, 1955
Doolin, Brian F Smith, G Allan Drinkwater, Fred J , III; An air-borne target simulator for use in optical sight tracking studies; naca-rm-a55f20; September 1955
Scherrer, Richard., Gowen, Forrest E.; Preliminary experimental investigation of a variable-area, variable-internal-contraction air inlet at Mach numbers between 1.42 and 2.44; naca-rm-a55f23; 1955
Warner Robert W.; Comparison between analytical and wind-tunnel results on flutter of several low-aspect-ratio, high-density, unswept wings at high subsonic speeds and zero angle of attack; naca-rm-a55g08; 1955
Boyd, John W., Migotsky, Eugene., Wetzel, Benton E.; A study of conical camber for triangular and sweptback wings; naca-rm-a55g19; 1955
Wetzel, Benton E.; Effect of leading-edge sweepback on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 and taper ratio 0.4 at subsonic and supersonic speeds; naca-rm-a55h04a; 1955
Wong, Thomas J., Gloria, Hermilo R.; Aerodynamic characteristics of two rectangular-plan-form, all moveable controls in combination with a slender body of revolution at Mach numbers from 3.00 to 6.25; naca-rm-a55j07; 1955
Coe, Charles F.; A study of local-pressure fluctuations relative to static-pressure distributions on two-dimensional airfoils at high subsonic Mach numbers; naca-rm-a55j11; 1955
Jack D. Stephenson, Angelo Bandettini, and Ralph Selan (Ames Aeroanutical Laboratory, Moffett Field Calif.); Longitudinal Stability Characteristics at Mach Numbers up to 0.92 of a Wing-Body-Tail Combination Having a Wing with 45o of Sweepback and a Tail in Various Vertical Positions; naca-rm-a54k09; 1955

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