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- 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
- Cylinder-head temperatures and coolant heat rejection of a multicylinder liquid-cooled engine of 1650-cubic-inch displacement
- Comparison of theoretical and experimental heat transfer on a cooled 20 degrees cone with a laminar boundary layer at a Mach number of 2.02
- A comparison of theoretical and experimental wing bending moments during seaplane landings
- Effect of an unswept wing on the contribution of unswept-tail configuration to the low-speed static and rolling-stability derivatives of a midwing airplane model
- Effect of aspect ratio on the air forces and moments of harmonically oscillating thin rectangular wings in supersonic potential flow
- The development and performance of two small tunnels capable of intermittent operation at Mach numbers between 0.4 and 4.0
- Investigation of spark-over voltage - density relation for gas-temperature sensing
- Application of the wire-mesh plotting device to incompressible cascade flows
- Relation Between Inflammables and Ignition Sources in Aircraft Environments
- A flight investigation and analysis of the lateral-oscillation characteristics of an airplane
- Stress and distortion measurements in a 45 degree swept box beam subjected to antisymmetrical bending and torsion
- Stress and strain concentration at a circular hole in an infinite plate
- Spectrums and diffusion in a round turbulent jet
- Spin-tunnel investigation to determine the effect on spin recoveries of reducing the opening shock load of spin-recovery parachutes
- The calculation of downwash behind wings of arbitrary plan form at supersonic speeds