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- Horizontal tail loads in maneuvering flight
- A numerical procedure for designing cascade blades with prescribed velocity distribution in incompressible potential flow
- Friction and wear of hot-pressed bearing materials containing molybdenum disulfide
- Interferometer corrections and measurements of laminar boundary layers in supersonic stream
- Investigation of a NACA high-speed optical torquemeter
- Investigation of a NACA high-speed strain-gage torquemeter
- Investigation of properties of AISI type 310B alloy sheet at high temperatures
- Method of analysis for compressible flow through mixed-flow centrifugal impellers of arbitrary design
- A method of calibrating airspeed installations on airplanes at transonic and supersonic speeds by use of temperature measurements
- Method of calculating the lateral motions of aircraft based on the Laplace transform
- A method of computing subsonic flows around given airfoils
- Wind-tunnel investigation at low speed of a 45 degree sweptback untapered semispan wing of aspect ratio 1.59 equipped with various 25-percent chord plain flaps
- Wind-tunnel investigation at low speed of an unswept untapered semispan wing of aspect ratio 3.13 equipped with various 25-percent-chord plain flaps
- Wind-tunnel investigation at low speed of the lateral control characteristics of an unswept untapered semi-span wing of aspect ratio 3.13 equipped with various 25-percent-chord plain ailerons
- Static and impact strengths of riveted and spot-welded beams of Alclad 14S-T6, Alclad 75S-T6, and various tempers of Alclad 24S aluminum alloy
- Experimental analysis of a pressure-sensitive system for sensing gas temperature
- Lift-cancellation technique in linearized supersonic-wing theory
- The load distribution due to sideslip on triangular, trapezoidal, and related plan forms in supersonic flow
- Low-speed characteristics of four cambered, 10-percent-thick NACA airfoil sections
- Low-speed investigation of a thin, faired, double-wedge airfoil section with nose flaps of various chords
- Measurement of the moments of inertia of an airplane by a simplified method
- Floating characteristics of rudders and elevators in spinning attitudes as determined from hinge-moment-coefficient data with application to personal-owner-type airplanes
- Impact-pressure interpretation in a rarefied gas at supersonic speeds
- Friction of surface films formed by decomposition of common lubricants of several types
- On the effect of subsonic trailing edges on damping in roll and pitch of thin sweptback wings in a supersonic stream
- On the particular integrals of the Prandtl-Busemann iteration equations for the flow of a compressible fluid
- Effect of chemical reactivity of lubricant additives on friction and surface welding at high sliding velocities
- Correlation of effects of fuel-air ratio, compression ratio, and inlet-air temperature on knock limits of aviation fuels
- Correlation of physical properties with molecular structure for dicyclic hydrocarbons : I -2-n-alkylbiphenyl, 1,1-diphenylalkane,a,w-diphenylalkane; 1,1-dicyclohexylalkane, and a,w-dicyclohexylalkane series
- Correlations of heat-transfer data and of friction data for interrupted plane fins staggered in successive rows
- A determination of the laminar-, transitional-, and turbulent-boundary-layer temperature-recovery factors on a flat plate in supersonic flow
- The design, operation, and uses of the water channel as an instrument for the investigation of compressible-flow phenomena
- Theoretical calculations of the supersonic pressure distribution and wave drag for a limited family of tapered sweptback wings with symmetrical parabolic-arc sections at zero lift
- Comparison between theory and experiment for wings at supersonic speeds
- Comparison of fatigue strengths of bare and Alclad 24S-T3 aluminum-alloy sheet specimens tested at 12 and 1000 cycles per minute
- Comparative foaming characteristics of aeronautical lubricating oils
- Analysis of shear strength of honeycomb cores for sandwich constructions
- Bending and buckling of rectangular sandwich plates
- Comparison of model and full-scale spin test results for 60 airplane designs
- Analysis of factors influencing the stability characteristics of symmetrical twin-intake Air-induction systems
- Compressive properties of titanium sheet at elevated temperatures
- Analysis of effect of variations in primary variables on time constant and turbine-inlet-temperature overshoot of turbojet engine
- The boundary-layer and stalling characteristics of the NACA 64A010 airfoil section
- Boundary-layer transition on a cooled 20 degree cone at Mach numbers of 1.5 and 2.0
- Effect of variation in rivet diameter and pitch on the average stress at maximum load for 24S-T3 and 75S-T6 aluminum-alloy, flat, Z-stiffened panels that fail by local instability
- Effect of tunnel configuration and testing technique on cascade performance
- Determination of the rate of roll of pilotless aircraft research models by means of polarized radio waves
- Effect of valve overlap and compression ratio on variation of measured performance with exhaust pressure of aircraft cylinder and on computed performance of compound power plant
- Effects of modifications to the leading-edge region on the stalling characteristics of the NACA 63(sub 1)-012 airfoil section
- Effectiveness of molybdenum disulfide as a fretting-corrosion inhibitor