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- Effect of open circular holes on tensile strength and elongation of sheet specimens of a magnesium alloy
- A survey of the aircraft-noise problem with special reference to its physical aspects
- The theoretical characteristics of triangular-tip control surfaces at supersonic speeds: Mach lines behind trailing edges
- Two-dimensional flow on general surfaces of revolution in turbomachines
- Some effects of varying the damping in pitch and roll on the flying qualities of a small single-rotor helicopter
- Investigation of the influence of fuselage and tail surfaces on low-speed static stability and rolling characteristics of a swept-wing model
- Critical study of integral methods in compressible laminar boundary layers
- Buckling of rectangular sandwich plates subjected to edgewise compression with loaded edges simply supported and unloaded edges clamped
- Calculation of aerodynamic forces on a propeller in pitch or yaw
- Electrical techniques for compensation of thermal time lag of thermocouples and resistance thermometer elements
- Effects of Aspect Ratio on Air Flow at High Subsonic Mach Numbers
- An approximate method of determining the subsonic flow in an arbitrary stream filament of revolution cut by arbitrary turbomachine blades
- Wing-body interference at supersonic speeds with an application to combinations with rectangular wings
- Flame speeds of 2,2,4-trimethylpentane-oxygen-nitrogen mixtures
- Torsion tests of aluminum-alloy stiffened circular cylinders
- Flow surfaces in rotating axial-flow passages
- Fundamental effects of cold-work on some cobalt-chromium-nickel-iron base creep-resistant alloys
- A fundamental study of the mechanism by which hydrogen enters metals during chemical and electrochemical processing
- Investigation of laminar boundary layer in compressible fluids using the Crocco method
- The similarity law for nonsteady hypersonic flows and requirements for the dynamical similarity of related bodies in free flight
- Investigation of a diffraction-grating interferometer for use in aerodynamic research
- Interaction between a supersonic stream and a parallel subsonic stream bounded by fluid at rest
- Interaction of oblique shock waves with regions of variable pressure, entropy, and energy
- Instrument-flight results obtained with a combined-signal flight indicator modified for helicopter use
- Investigation of stress distribution in rectangular plates with longitudinal stiffeners under axial compression after buckling
- Investigation of spontaneous ignition temperatures of organic compounds with particular emphasis on lubricants
- Investigation of statistical nature of fatigue properties
- A method for finding a least-squares polynomial that passes through a specified point with specified derivatives
- Measurements of flying qualities of an F-47D-30 airplane to determine lateral and directional stability and control characteristics
- A method for the determination of the time lag in pressure measuring systems incorporating capillaries
- Noise from intermittent jet engines and steady-flow jet engines with rough burning
- The Langley 2,000-horsepower propeller dynamometer and tests at high speed of an NACA 10-(3)(08)-03 two-blade propeller
- Principle and application of complementary energy method for thin homogeneous and sandwich plates and shells with finite deflections
- Langley full-scale-tunnel investigations of the maximum-lift and stalling characteristics of a trapezoidal wing of aspect ratio 4 with circular-arc airfoil sections
- Laminar natural-convection flow and heat transfer of fluids with and without heat sources in channels with constant wall temperatures
- Flame speeds of methane-air, propane-air, and ethylene-air mixtures at low initial temperatures
- General consideration of problems in compressible flow using the hodograph method
- Theoretical analysis of hydrodynamic impact of a prismatic float having freedom in trim
- One-dimensional compressible flow in vaneless diffusers of radial- and mixed-flow centrifugal compressors, including effects of friction, heat transfer and area change
- Determination of indicial lift and moment of a two-dimensional pitching airfoil at subsonic mach numbers from oscillatory coefficients with numerical calculations for a Mach number of 0.7
- Effect of changing passage configuration on internal-flow characteristics of a 48-inch centrifugal compressor II : change in hub shape
- Corrosion of magnesium alloy ZK60A in marine atmosphere and tidewater
- Design of two-dimensional channels with prescribed velocity distribution along the channel walls I : relaxation solutions
- Three-dimensional supersonic nozzles and inlets of arbitrary exit cross section
- Calorimetric determination of constant-pressure specific heats of carbon dioxide at elevated pressures and temperatures
- A comparative examination of some measurements of airfoil section lift and drag at supercritical speeds
- Behavior of vortex system behind cruciform wings - motions of fully rolled-up vortices
- Analysis of Landing-Gear Behavior
- An analysis of normal accelerations and airspeeds of one type of twin-engine transport airplane in commercial operations over a northern transcontinental route
- Compressive buckling of simply supported curved plates and cylinders of sandwich construction