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- Investigation of the effects of profile shape on the aerodynamic and structural characteristics of thin, two-dimensional airfoils at supersonic speeds
- Flight investigation of pentaborane fuel in rocket boosted 9.75-inch-diameter ramjet engine with convergent-divergent exhaust nozzle
- Flight investigation of pentaborane fuel in 9.75-inch-diameter ram-jet engine with downstream fuel injection
- Free-flight skin-temperature and surface-pressure measurements on a highly polished nose having a 100 degree total-angle cone and a 10 degree half-angle conical flare section up to a Mach number of 4.08
- Screen-type noise reduction devices for ground running of turbojet engines
- In-flight gains realized by modifying a twin side-inlet induction system
- Investigation at transonic speeds of deflectors and spoilers as gust alleviators on a 35 degree swept wing: transonic bump method
- Investigation of 70 percent trimethyl borate 30 percent methyl alcohol fuel mixture in a single J33 combustor and in a J33 turbojet engine
- Induced velocities near a lifting rotor with nonuniform disk loading
- Investigation at transonic speeds of loading over a 30 degree sweptback wing of aspect ratio 3, taper ratio 0.2, and NACA 65A004 airfoil section mounted on a body
- A theoretical and experimental study of boric oxide deposition on a surface immersed in an exhaust gas stream from a jet-engine combustor, including a method of calculating deposition
- A theory for the lateral response of airplanes to random atmospheric turbulence
- Theoretical and experimental investigations of delta-wing vibrations
- The subsonic static aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3. II : lateral and directional characteristics
- The subsonic static aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3. I : effects of horizontal-tail location and size on the longitudinal characteristics
- The subsonic static aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3. III : effects of trailing-edge flaps
- Transonic wind-tunnel investigation of the low-lift aerodynamic characteristics, including the effects of leading edge droop and thickness, of a thin trapezoidal wing in combination with basic and indented bodies
- A summary of ground-loads statistics
- Theory of aircraft structural models subject to aerodynamic heating and external loads
- Theory of Self-Excited Mechanical Oscillations of Helicopter Rotors with Hinged Blades
- Theoretical investigation of the effects of configuration changes on the center-of-pressure shift of a body-wing-tail combination due to angle of attack and mach number at transonic speeds
- Altitude performance of a full-scale turbojet engine using pentaborane fuels
- Altitude performance of a turbojet engine using pentaborane fuel
- Altitude performance of pentaborane - JP-4 fuel blends in a modified J47 combustor
- Two-dimensional transonic investigation of flows and forces on a 9-percent-thick airfoil with 30-percent-chord flap
- Turbulence measurements in multiple interfering air jets
- Theory and design of a pneumatic temperature probe and experimental results obtained in a high-temperature gas stream
- A theoretical study of the aerodynamics of slender cruciform-wing arrangements and their wakes
- A theoretical study of the effect of upstream transpiration cooling on the heat-transfer and skin-friction characteristics of a compressible, laminar boundary layer
- Transition-flight investigation of a four-engine-transport vertical-take-off airplane model utilizing a large flap and extensible vanes for redirecting the propeller slipstream
- Theory and apparatus for measurement of emissivity for radiative cooling of hypersonic aircraft with data for Inconel and Inconel X
- Low-speed pressure-distribution investigation of a thin-delta-wing-fuselage model having double slotted flaps and spoilers
- The linearized subsonic flow about symmetrical nonlifting wing-body combinations
- Methods for obtaining desired helicopter stability characteristics and procedures for stability predictions
- A method utilizing data on the spiral, roll-subsidence, and dutch roll modes for determining lateral stability derivatives from flight measurements
- Momentum transfer for flow over a flat plate with blowing
- Practical solution of plastic deformation problems in elastic-plastic range
- Rupture strength of several nickel-base alloys in sheet form
- NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results
- Performance and operational characteristics of pentaborane fuel in 48-inch-diameter ram-jet engine
- Perforated sheets as the porous material for a suction-flap application
- 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
- A rapid method for predicting attached-shock shape
- Reaction of fluorine with carbon as a means of fluorine disposal
- Some data on body and jet reaction controls
- Some characteristics of roll controls having possible application to fin-stabilized ammunition
- Performance evaluation of reduced-chord rotor blading as applied to J73 two-stage turbine II : over-all performance at inlet conditions of 35 inches of mercury absolute and 700 R
- Performance evaluation of reduced-chord rotor blading as applied to J73 two-stage turbine V : effect of inlet pressure on over-all performance at design speed and inlet temperature of 700 R
- Performance evaluation of reduced-chord rotor blading as applied to J73 two-stage turbine IV : over-all performance of first-stage turbine with reduced-chord rotor blades at inlet conditions of 35 inches of mercury absolute and 700 R
- Performance of 110-millimeter-bore M-1 tool steel ball bearings at high speeds, loads, and temperatures