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- A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results
- Analytical determination of coupled bending-torsion vibrations of cantilever beams by means of station functions
- Generalization of Joukowski formula to an airfoil of a cascade in compressible gas stream with subsonic velocities
- Effect of aspect ratio on the air forces and moments of harmonically oscillating thin rectangular wings in supersonic potential flow
- Analysis of the effects of boundary-layer control in the take-off and power-off landing performance characteristics of a liaison type of airplane
- Relation between inflammables and ignition sources in aircraft environments
- Spectra and diffusion in a round turbulent jet
- Calculation of the lateral control of swept and unswept flexible wings of arbitrary stiffness
- An empirically derived basis for calculating the area, rate, and distribution of water-drop impingement on airfoils
- Diffusion of chromium in alpha cobalt-chromium solid solutions
- A theoretical analysis of the effect of time lag in an automatic stabilization system on the lateral oscillatory stability of an airplane
- Error in Airspeed Measurement Due to Static-Pressure Field Ahead of the Wing Tip of a Swept-Wing Airplane Model at Transonic Speeds
- A biharmonic relaxation method for calculating thermal stress in cooled irregular cylinders
- Spectrum of turbulence in a contracting stream
- Analysis of the effects of wing interference on the tail contributions to the rolling derivatives
- Exploratory investigation at high and low subsonic Mach numbers of two experimental 6-percent-thick airfoil sections designed to have high maximum lift coefficients
- A flight study of requirements for satisfactory lateral oscillatory characteristics of fighter aircraft
- Flow separation ahead of a blunt axially symmetric body at Mach numbers 1.76 to 2.10
- Effects on control effectiveness of systematically varying the size and location of trailing-edge flaps on a 45 degrees sweptback wing at a Mach number of 1.9
- Fundamental aging effects influencing high-temperature properties of solution-treated Inconel X
- Fundamental flame velocities of pure hydrocarbons III : extension of tube method of high flame velocities - acetylene-air mixtures
- Investigation of a triangular wing in conjunction with a fuselage and horizontal tail to determine downwash and longitudinal-stability characteristics: transonic bump method
- :Investigation of a 24-inch shock-in-rotor type supersonic compressor designed for simple radial equilibrium behind normal shock
- Investigation of turbines suitable for use in a turbojet engine wtih high compressor ratio and low compressor-tip speed V : experimental performance of two-stage turbine with downstream stator
- Investigation of wing-tip ailerons on a 51.3 degrees sweptback wing at transonic speeds by the transonic-bump method
- A method for the design of sweptback wings warped to produce specified flight characteristics at supersonic speeds
- Preliminary investigation of a translating cowl technique for improving take-off performance of a sharp-lip supersonic diffuser
- Method for estimating lift interference of wing-body combinations at supersonic speeds
- Performance of single-stage compressor designed on basis of constant total enthalpy with symmetrical velocity diagram at all radii and velocity ratio of 0.7 at rotor hub / Jack R. Burtt and Robert J. Jackson
- Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect ratio 4 triangular wing and an all-movable horizontal tail - longitudinal characteristics
- Preliminary evaluation of the air and fuel specific-impulse characteristics of several potential ram-jet fuels IV : hydrogen, a-methylnaphthalene, and carbon / Benson E. Gammon
- Preliminary results of turbojet-engine altitude-starting investigation
- Preliminary study of stability of flow from two ducts discharging into a common duct
- A summary of available knowledge concerning skin friction and heat transfer and its application to the design of high-speed missiles
- A preliminary investigation of combustion with rotating flow in an annular combustion chamber
- Pressure distribution at low speed on a 1/4-scale Bell X-5 airplane model
- Load distribution over a fuselage in combination with a swept wing at small angles of attack and transonic speeds
- Liquid-fuel-distribution and fuel-state effects on combustion performance of a single tubular combustor
- Flame velocities over a wide composition range for pentane-air, ethylene-air, and propyne-air flames
- The similarity law for hypersonic flow and requirements for dynamic similarity of related bodies in free flight
- Full-scale investigation of cooling shroud and ejector nozzle for a turbojet engine: afterburner installation
- Free-spinning tunnel investigation of the 1/21-scale model of the Chance Vought F7U-3 airplane: TED No. NACA DE 362
- Optical methods involving light scattering for measuring size and concentration of condensation particles in supercooled hypersonic flow
- Correlation of analog solutions with experimental sea-level transient data for controlled turbine-propeller engine, including analog results at altitudes
- Analytical investigation of flow through high-speed mixed-flow turbine
- Aerodynamic characteristics of a slender cone-cylinder body of revolution at a Mach number of 3.85
- Characteristics of a transonic test section with various slot shapes in the Langley 8-foot high-speed tunnel
- An analysis of base pressure at supersonic velocities and comparison with experiment
- Evaluation of the reduced-mass method of representing wing-lift effects in free-fall drop tests of landing gears
- System analyses and autopilot design for automatic roll stabilization of a supersonic pilotless aircraft