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- The effect of rate of change of angle of attack on the maximum lift of a small model
- Estimation of the damping in roll of supersonic-leading-edge wing-body combinations
- Experimental investigation of stiffened circular cylinders subjected to combined torsion and compression
- Experimental investigation of the effect of vertical-tail size and length of fuselage shape and length on the static lateral stability characteristics of a model with 45 degree sweptback wing and tail surfaces
- Experiments in external noise reduction of light airplanes
- Tables of wing-aileron coefficients of oscillating air forces for two-dimensional supersonic flow
- Statistical explanation of spontaneous freezing of water droplets
- Supersonic flow around circular cones at angles of attack
- Resistance of six cast high-temperature alloys to cracking caused by thermal shock
- Study of effects of sweep on the flutter of cantilever wings
- A small-deflection theory for curved sandwich plates
- Sound measurements for five shrouded propellers at static conditions
- Spanwise loading for wings and control surfaces of low aspect ratio
- Static longitudinal stability and control of a convertible-type airplane as affected by articulated-and rigid-propeller operation
- Propeller flight investigation to determine the effects of blade loading
- Synthesis and purification of alkyldiphenylmethane hydrocarbons 1: 2-methyldiphenylmethane, 3-methyldiphenylmethane, 2-ethyldiphenylmethane, 4-ethyldiphenylmethane and 4-isopropyldiphenylmethane
- Dynamic similitude between a model and a full-scale body for model investigation at full-scale Mach number
- Dynamics of a turbojet engine considered as a quasi-static system
- Improvement of high-temperature properties of magnesium-cerium forging alloys
- Investigation of 75-millimeter-bore cylindrical roller bearings at high speeds 2: lubrication studies - effect of oil-inlet location, angle, and velocity for single-jet lubrication
- An investigation of aircraft heaters XXXIII : experimental determination of thermal and hydrodynamical behavior of air flowing along finned plates
- Investigation of 75-millimeter-bore cylindrical roller bearings at high speeds: 1: Initial studies
- Stress and distortion analysis of a swept box beam having bulkheads perpendicular to the spars
- Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tipssupersonic leading edges
- Theoretical effect of inlet hub-tip-radius ratio and design specific mass flow on design performance of axial-flow compressors
- Turbojet thrust augmentation by evaporation of water prior to mechanical compression as determined by use of psychrometric chart
- Theoretical investigation and application of transonic similarity law for two dimensional flow
- Theory of helicopter damping in pitch or roll and a comparison with flight measurements
- Theoretical supersonic characteristics of inboard trailing-edge flaps having arbitrary sweep and taper: Mach lines behind flap leading and trailing edges
- Theoretical wave drags and pressure distributions for axially symmetric open-nose bodies
- Time-dependent downwash at the tail and the pitching moment due to normal acceleration at supersonic speeds
- Low-speed investigation of the stalling of a thin, faired, double-wedge airfoil with nose flap
- A method of determining the effect of airplane stability on the gust load factor
- Method of experimentally determining radial distributions of velocity through axial-flow compressor
- Effect of heat and power extraction on turbojet-engine performance 1: analytical method of performance evaluation with compressor-outlet air bleed
- Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces
- Effect of heat and power extraction on turbojet-engine performance 2: effect of compressor-outlet air bleed for specific modes of engine operation
- Effect of heat and power extraction on turbojet-engine performance 3: analytical determination of effects of shaft-power extraction
- Formulas for source, doublet, and vortex distributions in supersonic wing theory
- Chart for simplifying calculations of pressure drop of a high-speed compressible fluid under simultaneous action of friction and heat transfer - application to combustion-chamber cooling passages
- The interpretation of biaxial-tension experiments involving constant stress ratios
- An experimental investigation of the NACA 631-012 airfoil section with leading-edge and midchord suction slots
- An analysis of the normal accelerations and airspeeds of a four-engine airplane type in postwar commercial transport operations on trans-Pacific and Caribbean-South American routes
- An approximate method of calculating pressures in the tip region of a rectangular wing of circular-arc section at supersonic speeds
- Approximate aerodynamic influence coefficients for wings of arbitrary plan form in subsonic flow
- Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds : supersonic leading and trailing edges
- The effects of stability of spin-recovery tail parachutes on the behavior of airplanes in gliding flight and in spins
- Frequency response of positive-displacement variable stroke fuel pump
- Investigation of the flow through a single-stage two-dimensional nozzle in the Langley 11-inch hypersonic tunnel
- Critical stress of plate columns