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- Synthesis of cyclopropane hydrocarbons from methylcyclopropyl ketone 3: 2-cyclopropyl-1-butene, cis and trans 2-cyclopropyl-2-butene, and 2-cyclopropylbutane
- Synthesis, purification and physical properties of hydrocarbons of the naphthalene series 1: 1-methylnaphthalene, 1-ethylnaphthalene, 1-butylnaphthalene, and 1-isobutylnaphthalene
- An improved approximate method for calculating lift distributions due to twist
- Experimental study of an angle-of-attack vane mounted ahead of the nose of an airplane for use as a sensing device for an acceleration alleviator
- Flight investigation of some factors affecting the critical tail loads on large airplanes
- Flight investigation of the effect of transient wing response on wing strains of a twin-engine transport airplane in rough air
- General plastic behavior and approximate solutions of rotating disk in strain-hardening range
- An investigation of aircraft heaters XXXVIII : determination of thermal performance of rectangular- and trapezoidal-shaped inner-skin passages for anti-icing systems
- The Indicial Lift and Pitching Moment for a Sinking or Pitching Two-Dimensional Wing Flying at Subsonic or Supersonic Speeds
- Inelastic column behavior
- Theoretical characteristics of two-dimensional supersonic control surfaces
- Theoretical force and moments due to sideslip of a number of vertical tail configurations at supersonic speeds
- Two axial-symmetry solutions for incompressible flow through a centrifugal compressor with and without inducer vanes
- Unsteady laminar boundary-layer flow
- The use of an uncalibrated cone for determination of flow angles and Mach numbers at supersonic speeds
- Linearized solution and general plastic behavior of thin plate with circular hole in strain-hardening range
- Method of matching components and predicting performance of turbine-propeller engine
- A method of solving the direct and inverse problem of supersonic flow along arbitrary stream filaments of revolution in turbomachines
- Rupture properties of low carbon N-155 type alloys made with a columbium-tantalum ferro-alloy
- Stability and control characteristics of a complete airplane model having a wing with quarter-chord line swept back 40 degrees, aspect ratio 2.50, and taper ratio 0.42
- Formation of sulfide films on steel and effect of such films on static friction
- Automatic control systems satisfying certain general criterions on transient behavior
- Charts and tables for use in calculations of downwash of wings of arbitrary plan form
- Empirical Relation Between Induced Velocity, Thrust, and Rate of Descent of a Helicopter Rotor as Determined by Wind-Tunnel Tests on Four Model Rotors
- Fatigue strengths of aircraft materials: axial load fatigue tests on unnotched sheet specimens of 24S-T3 and 75S-T6 aluminum alloys and of SAE 4130 steel
- Fatigue strengths of aircraft materials: axial-load fatigue tests on notched sheet specimens of 24S-T3 and 75S-T6 aluminum alloys and of SAE 4130 steel with stress-concentration factor of 5.0
- Effect of tail surfaces on the base drag of a body of revolution at Mach numbers of 1.5 and 2.0
- Influence of refraction on the applicability of the Zehnder-Mach interferometer to studies of cooled boundary layers
- Laminar boundary layer on a circular cone in supersonic flow at a small angle of attack
- Effect of taper ratio on the low-speed rolling stability derivatives of swept and unswept wings of aspect ratio 2.61
- Jet-boundary corrections for complete and semispan swept wings in closed circular wind tunnels
- Effect of ground interference on the aerodynamic characteristics of a 42 degrees sweptback wing
- A numerical approach to the instability problem of monocoque cylinders
- Method for calculation of ram-jet performance
- Method for determining pressure drop of monatomic gases flowing in turbulent motion through constant-area passages with simultaneous friction and heat addition
- An investigation of the effects of jet-outlet cut-off angle on thrust direction and body pitching moment
- Pilot escape from spinning airplanes as determined from free-spinning-tunnel tests
- A plan-form parameter for correlating certain aerodynamic characteristics of swept wings
- Temperature distribution in internally heated walls of heat exchangers with noncircular flow passages using coolants with very low Prandtl number
- Stresses in a two-bay noncircular cylinder under traverse loads
- Some effects of variations in several parameters including fluid density on the flutter speed of light uniform cantilever wings
- Three-dimensional compressible laminar boundary-layer flow
- Approximate design method for high-solidity blade elements in compressors and turbines
- An Analytical and Experimental Investigation of the Skin Friction of the Turbulent Boundary Layer on a Flat Plate at Supersonic Speeds
- Generalized conical-flow fields in supersonic wing theory
- Effects on longitudinal stability and control characteristics of a B-29 airplane of variations in stick-force and control-rate characteristics obtained through use of a booster in the elevator-control system
- The effect of an arbitrary surface-temperature variation along a flat plate on the convective heat transfer in an incompressible turbulent boundary layer
- Application of the Von Kármán momentum theorem to turbulent boundary layers
- Wind-tunnel tests at low speed of swept and yawed wings having various plan forms
- Regenerator-design study and its application to turbine-propeller engines