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- Low-speed experimental investigation of the magnus effect on various sections of a body of revolution with and without a propeller
- Measurement of static pressure on aircraft
- Measurement of aerodynamic forces for various mean angles of attack on an airfoil oscillating in pitch and on two finite-span wings oscillating in bending with emphasis on damping in the stall
- The measurement of pressure altitude on aircraft
- Exploratory study of ground proximity effects on thrust of annular and circular nozzles
- Results of the flight test of a 0.13-scale rocket-boosted model of the McDonnell F4H-1 airplane between Mach numbers of 0.20 and 1.90: TED No. NACA AD 3115
- Flight tests of an automatic interceptor system with a tracking radar modified to minimize the interaction between antenna and interceptor motions
- Exploratory investigation of aerodynamic effects of external combustion of aluminum borohydride in airstream adjacent to flat plate in Mach 2.46 tunnel
- Full-scale free-jet investigation of a two-shock side-inlet diffuser at Mach 2.75 and a comparison with a single-shock diffuser
- Impact-loads investigation of chine-immersed models having concave-convex transverse shape and straight or curved keel lines
- Impact-loads investigation of a chine-immersed model having a longitudinally curved bow and a v-bottom with a dead-rise angle of 30 degrees
- Heat transfer and boundary-layer transition on two blunt bodies at Mach numbers 3.12
- Heat transfer and recovery temperatures on a sphere with laminar, transitional, and turbulent boundary layers at Mach numbers of 2.00 and 4.15
- Heat-exchanger-core weights for use with hydrogen expansion turbine
- A note on the effect of heat transfer on peak pressure rise associated with separation of turbulent boundary layer on a body of revolution (NACA RM-10) at a Mach number of 1.61
- Investigation of a nonlinear control system
- Preliminary investigation of the characteristics of a two dimensional wing and propeller with the propeller plane of rotation in the wing-chord plane
- Investigation of a nonlinear control system
- Recent research on the creep of airframe components
- Applications of power spectral analysis methods to maneuver loads obtained on jet fighter airplanes during service operations
- Effect of fiber orientation on ball failures under rolling-contact conditions
- Effect of crystal orientation on fatigue-crack initiation in polycrystalline aluminum alloys
- Arrangements of jet engine and airframe for increased range
- Effect of fuel properties on liner temperatures in a single tubular turbojet combustor
- Creep behavior of structural joints of aircraft materials under constant loads and temperatures
- Creep deformation patterns of joints under bearing and tensile loads
- Drop burning rates of hydrocarbon and nonhydrocarbon fuels
- Effect of lubricant viscosity on rolling-contact fatigue life
- Effect of nose shape on subsonic aerodynamic characteristics of a body of revolution having a fineness ratio of 10.94
- Effect of overheating on creep-rupture properties of HS-31 alloy at 1,500 F
- Analytical investigation of the effect of water injection on supersonic turbojet-engine - inlet matching and thrust augmentation
- Analytical study of the comparative pitch-up behavior of several airplanes and correlation with pilot opinion
- Calculated and measured stresses in simple panels subject to intense random acoustic loading including the near noise field of a turbojet engine
- Cascade investigation of cooling characteristics of a cast-finned air-cooled turbine blade for use in a turboprop engine
- A comparison of carrier approach speeds as determined from flight tests and from pilot-operated simulator studies
- Comparison of calculated and experimental load distributions on thin wings at high subsonic and sonic speeds
- Comparison of effect of a turbojet engine and three cold-flow configurations on the stability of a full-scale supersonicle inlet
- Combustor performance of a 16-inch ram jet using gaseous hydrogen as fuel at Mach number 3.0
- An analytical investigation of the gust-alleviating properties of a simple pitch damper
- Analysis of operational airline data to show the effects of airborne weather radar on the gust loads and operating practices of twin-engine short-haul transport airplanes
- Flight tests of a model of a high-wing transport vertical-take-off airplane with tilting wing and propellers and with jet controls at the rear of the fuselage for pitch and yaw control
- Comparison of NACA 65-series compressor-blade pressure distributions and performance in a rotor and in cascade
- Analysis of experimental low-speed loss and stall characteristics of two-dimensional compressor blade cascades
- Analysis of fluorine addition to the vanguard first stage
- Analysis of horizontal-tail loads in pitching maneuvers on a flexible swept-wing jet bomber
- Characteristics of a 40 degree cone for measuring Mach number, total pressure, and flow angles at supersonic speeds
- The combinations of thermal and load stresses for the onset of permanent buckling in plates
- Comparison of experimental with theoretical total-pressure loss in parallel-walled turbojet combustors
- Component performance investigation of J71 experimental turbine VII: effect of first-stator adjustment; over-all performance of J71 turbine with 87-percent-design stator area
- Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number