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- Aerodynamic characteristics at high speeds of full-scale propellers having Clark Y blade sections
- Low-speed pressure distributions over the drooped-nose flap of a 42 degrees sweptback wing with circular-arc airfoil sections at a Reynolds number of 5.3 x 10(exp 6)
- Stability and control characteristics of a free-flying model with an unswept wing of aspect ratio 3 (XS-3)
- Performance investigation of can-type combustor 1: instrumentation, altitude operational limits and combustion efficiency
- Performance investigation of can-type combustor 2: water injection at various stations in combustor
- Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers 3: normal-shock diffuser
- Pressure recovery at supersonic speeds through annular duct inlets situated in a region of appreciable boundary layer I : addition of energy to the boundary layer
- Experimental determination of the lateral stability of a glider towed by a single towline and correlation with an approximate theory
- Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : subsonic Mach and Reynolds number effects on the characteristics of the wing and on the effectiveness of an elevon
- Empirical mode constants for calculating frequencies of axial-flow compressor blades
- Control requirements and control parameters for a ram jet with variable-area exhaust nozzle
- Accuracy of airspeed measurements and flight calibration procedures
- Investigation of the Aerodynamic and Icing Characteristics of a Recessed Fuel Cell Vent Assembly 1: Rear Wall Vent Tube Mounting
- Experimental investigation of hot-gas bleedback for ice protection of turbojet engines 1: nacelle with offset air inlet
- Investigation of the aerodynamic and icing characteristics of a recessed fuel cell vent assembly 3: NACA flush-inlet-type vent
- Some effects of gutter flame-holder dimensions on combustion-chamber performance of 20-inch ram jet
- Experimental investigation at supersonic speeds of twin-scoop duct inlets of equal area III : inlet enclosing 37.2 percent of the maximum circumference of the forebody
- Experimental investigation at supersonic speeds of twin-scoop duct inlets of equal area II : effects of slots upon an inlet enclosing 61.5 percent of the maximum circumference of the forebody
- Generalized charts for determination of pressure drop of a high-speed compressible fluid in heat-exchanger passages I : air heated in smooth passages of constant area with constant wall temperature
- Investigation of the I-40 jet-propulsion engine in the Cleveland altitude wind tunnel I : performance and windmilling drag characteristics
- Theoretical performance of some rocket propellants containing hydrogen, nitrogen, and oxygen
- Comparison of two fuels in bumblebee 18-inch ram jet incorporating rake-type flame holder
- Effect of leading-edge high-lift devices and split flaps on the maximum-lift and lateral characteristics of a rectangular wing of aspect ratio 3.4 with circular-arc airfoil sections at Reynolds numbers from 2.9 x 10(exp 6) to 8.4 x 10(exp 6)
- Design and performance of experimental axial-discharge mixed-flow compressor I : impeller design theory
- Inlet Icing and Effectiveness of Hot-Gas Bleedback for Ice Protection of Turbojet Engine
- Application of one part of Von Karman's two-dimensional transonic similarity law to drag data of NACA 65-series wings
- Axial fatigue tests at zero mean stress of 24S-T and 75S-T aluminum-alloy strips with a central circular hole
- Wind-tunnel investigation of horizontal tails 3: unswept and 35 degrees swept-back plan forms of aspect ratio 6
- Investigation of wing characteristics at a Mach number of 1.53 3: unswept wings of differing aspect ratio and taper ratio
- Investigation of wing characteristics at a Mach number of 1.53 2: swept wings of taper ratio 0.5
- Calculation of the aerodynamic loading of swept and unswept flexible wings of arbitrary stiffness
- Ram-recovery characteristics of NACA submerged inlets at high subsonic speeds
- Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers 1: shock diffuser with triple-shock projecting cone
- An exploratory investigation of the relative merits of split and chord-extension flaps on a 45 degrees swept-back wing
- Investigation of effects of movable exhaust-nozzle plug on operational performance of 20-inch ram jet
- Ditching tests of a 1/15-scale model of the Fairchild C-82 airplane
- An investigation at low speed of a 51.3 degrees sweptback semispan wing with a raked tip and with 16.7-percent-chord ailerons having three spans and three trailing-edge angles
- An investigation at low speed of a 51.3 degree sweptback semispan wing equipped with 16.7-percent-chord plain flaps and ailerons having various spans and three trailing-edge angles
- Free-flight investigation of 16-inch diameter supersonic ram-jet unit
- Free-flight investigation of the rolling effectiveness at high subsonic, transonic, and supersonic speeds of leading-edge and trailing-edge ailerons in conjunction with tapered and untapered plan forms
- Charts for the Computation of Equilibrium Composition of Chemical Reactions in the Carbon-Hydrogen-Nitrogen System at Temperatures from 2000 to 5000 Degrees K
- De-Icing Effectiveness of External Electric Heaters for Propeller Blades
- Preliminary Results of Natural Icing of an Axial-Flow Turbojet Engine
- Preliminary Wind-Tunnel Investigation of the Effect of Area Suction on the Laminar Boundary Layer Over an NACA 64A010 Airfoil
- Investigation of Boundary-Layer Reynolds Number for Transition on an NACA 65 (Sub 215)-114 Airfoil in the Langley Two-Dimensional Low-Turbulence Pressure Tunnel
- Investigation of the Penetration of an Air Jet Directed Perpendicularly to an Air Stream
- Sideslip Angles and Vertical-Tail Loads Developed by Periodic Control Deflections
- Theoretical Wave Drag and Lift of Thin Supersonic Ring Airfoils
- The Theoretical Lift of Flat Swept-Back Wings at Supersonic Speeds
- Theoretical Method for Solution of Aerodynamic Forces on Thin Wings in Nonuniform Supersonic Stream With an Application to Tail Surfaces