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- Low-speed measurements of tail contribution to rolling stability derivatives and air-flow angularity at the tail for an x-tail model in steady roll including some effects of wing-tip stores
- Low-speed investigation of the lateral-control characteristics of a flap-type spoiler and a spoiler-slot deflector on a 30 degree sweptback wing-fuselage model having an aspect ratio of 3, a taper ratio of 0.5, and NACA 65A004 airfoil section
- Low-Speed Static Stability Characteristics of a Complete Model with an M-Wing in Mid and High Positions and with Three Horizontal-Tail Heights
- Low-speed wind-tunnel results for a thin aspect-ratio-1.85 pointed-wing-fuselage model with double slotted flaps
- Methods for measuring temperatures of thin-walled gas-turbine blades
- Methods for calculating thrust augmentation and liquid consumption for various turbojet-afterburner fuels
- Minimum-drag ducted and closed three-point body of revolution based on linearized supersonic theory
- Minimum drag of the Chance Vought XF8U-1 airplane as determined from the flight test of a 0.11-scale rocket-boosted model at Mach numbers between 0.73 and 1.71 : TED No. NACA DE 392
- Motion of a ballistic missile angularly misaligned with the flight path upon entering the atmosphere and its effect upon aerodynamic heating, aerodynamic loads, and miss distance
- Poisson's ratios and volume changes for plastically orthotropic material
- Seat design for crash worthiness
- Some considerations regarding the application of the supersonic area rule to the design of airplane fuselages
- Perforated sheets as a porous material for distributed suction and injection
- Performance characteristics of an axial-flow transonic compressor operating up to tip relative inlet Mach number of 1.34
- Performance characteristics of cylindrical target-type thrust reversers
- Rapid determination of core dimensions of crossflow gas-to-gas heat exchangers
- Radiation and recovery corrections and time constants of several chromel-alumel thermocouple probes in high-temperature, high-velocity gas streams
- Some effects of ailerons on the variation of aerodynamic characteristics with sideslip at low speed
- Some considerations of the influence of body cross-sectional shape on the lifting efficiency of wing-body combinations at supersonic speeds
- Some aspects of supersonic inlet stability
- Pressure distributions and aerodynamic characteristics of several spoiler-type controls on a trapezoidal wing at Mach numbers of 1.61 and 2.01
- Preliminary flight survey of aerodynamic noise on an airplane wing
- Preliminary investigation of self-excited vibrations of single planing surfaces
- Preliminary investigation of Guy alloy as a turbojet-engine bucket material for use at 1650 degrees F
- Stability of supersonic inlets at Mach 1.91 with air injection and suction
- Attenuation of tangential-pressure oscillations in a liquid-oxygen - n-heptane rocket engine with longitudinal fins
- Free-flight investigation at Mach numbers between 0.5 and 1.7 of the zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on an 80 degree delta-wing missile
- Calculations of the flow over an inclined flat plate at free-stream Mach number 1
- Average properties of compressible laminar boundary layer on flat plate with unsteady flight velocity
- Experimental determination of the range of applicability of the transonic area rule for wings of triangular plan form
- Effect of inlet-air-flow-distortions on steady-state performance of J65-B-3 turbojet engine
- Effect of inlet-duct length in uniform-flow field on turbojet-engine operation
- Effect of increase in angle of dead rise on the hydrodynamic qualities of a seaplane configuration incorporating high wing loading
- The influence of surface injection on heat-transfer and skin friction associated with the high-speed turbulent boundary layer
- Design of two transpiration-cooled strut-supported turbine rotor blades
- Aerodynamics of bodies, wings, and wing-body combinations at high angles of attack and supersonic speeds
- Afterburner performance with combustion-chamber lengths from 10 to 62 inches at several afterburner-inlet temperatures
- An analog study of the relative importance of various factors affecting roll coupling
- Experimental investigation of an overriding control to effect recovery from surge and stall in a turbojet engine
- Jet effects on base and afterbody pressures of a cylindrical afterbody at transonic speeds
- Investigation of the effects of body camber and body indentation on the longitudinal characteristics of a 60 degree delta-wing-body combination at a Mach number of 1.61
- A method for calculation of free-space sound pressures near a propeller in flight including considerations of the chordwise blade loading
- Method for calculating the aerodynamic loading on an oscillating finite wing in subsonic and sonic flow
- Method for calculating the aerodynamic loading on an oscillating finite wing in subsonic and sonic flow
- Low-speed longitudinal stability and lateral-control characteristics of a model of a 40 degree swept-wing fighter-type airplane at a Reynolds number of 9 x 10(exp 6)
- Preliminary investigation of short two-dimensional subsonic diffusers
- Preliminary investigation of the effects of external wing fuel tanks on ditching behavior of a sweptback-wing airplane
- Observation of laminar flow on a blunted 15 degree cone-cylinder in free flight at high reynolds numbers and free-stream mach numbers to 8.17
- Some effects of joint conductivity on the temperatures and thermal stresses in aerodynamically heated skin-stiffener combinations
- Temperature-control study of turbine region of turbojet engine, including turbine-blade time constants and starting characteristics