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- Aerodynamic characteristics at subsonic and supersonic Mach numbers of a thin triangular wing of aspect ratio 2 II : maximum thickness at midchord
- Static longitudinal aerodynamic characteristics of a 52 degree sweptback wing of aspect ratio 2.88 at Reynolds numbers from 2,000,000 to 11,000,000
- Study of stress states in gas-turbine disk as determined from measured operating-temperature distributions
- Tests of a triangular wing of aspect ratio 2 in the Ames 12-foot pressure wind tunnel III : the effectiveness and hinge moments of a skewed wing-tip flap
- Tests of a triangular wing of aspect ratio 2 in the Ames 12-foot pressure wind tunnel II : the effectiveness and hinge moments of a constant-chord plain flap
- Effect of a nacelle on the low-speed aerodynamic characteristics of a swept-back wing
- Investigation at supersonic speed (M = 1.53) of the pressure distribution over a 63 degrees swept airfoil of biconvex section at several angles of attack
- Investigation at supersonic speed (M = 1.53) of the pressure distribution over a 63 degrees swept airfoil of biconvex section at zero lift
- Tank spray tests of a jet-powered model fitted with NACA hydro-skis
- Tests of the NACA 64(sub 1)-012 and 64(sub 1)A012 airfoils at high subsonic Mach numbers
- Aerodynamic characteristics at high speeds of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller
- 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