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- Wing-dropping characteristics of some straight and swept wings at transonic speeds as determined with rocket-powered models
- Wing-flow measurements of longitudinal stability and control characteristics of a supersonic airplane configuration having a 42.8 degree sweptback circular arc wing with aspect ratio 4.0, taper ratio 0.50, and sweptback tail surfaces
- Approximate relative-total-pressure losses of an infinite cascade of supersonic blades with finite leading-edge thickness
- An experimental investigation of a jet-engine nacelle in several positions on a 37.25 degree swept-back wing
- Experimental investigation of a flat plate paddle jet vane operating on a rocket jet
- Low-temperature ignition-delay characteristics of several rocket fuels with mixed acid in modified open-cup-type apparatus
- Investigation of centrifugal compressor operated as a centripetal refrigeration turbine
- Cooling of ram jets and tail-pipe burners : analytical method for determining temperatures of combustion chamber having annular cooling passage
- The effects of compressibility on the pressures on a body of revolution and on the aerodynamic characteristics of a wing-nacelle combination consisting of the body of revolution mounted on a swept-back wing
- A comparison of the aerodynamic characteristics at transonic speeds of four wing-fuselage configurations as determined from different test techniques
- The effect of aspect ratio on the subsonic aerodynamic characteristics of wings with NACA 65(sub 1)-210 sections
- Effect of blade-root fit and lubrication on vibration characteristics of ball-root-type axial-flow-compressor blades
- A description of the design of highly swept propeller blades
- Effect of compressor-outlet bleedoff on turbojet-engine performance
- Application of blade cooling to gas turbines
- Investigation of downwash and wake characteristics at a Mach number of 1.53 3: swept wings
- Wind-tunnel tests of a 0.16-scale model of the X-3 airplane at high subsonic speeds: wing and fuselage pressure distribution
- Turbojet combustion efficiency at high altitudes
- Pressure-distribution and ram-recovery characteristics of NACA submerged inlets at high subsonic speeds
- Comparison of outside-surface heat-transfer coefficients for cascades of turbine blades
- Spontaneous ignition temperatures of pure hydrocarbons and commercial fluids
- Aeronautical study of a wing-fuselage combination employing a wing swept back 63 degrees: Characteristics at supersonic speeds of a model with the wing twisted and cambered for uniform load
- Investigation of the downwash and wake behind a triangular wing of aspect ratio 4 at subsonic and supersonic Mach numbers
- Investigation of effects of inlet-air velocity distortion on performance of turbojet engine
- Wind-tunnel investigation of a 1/6-scale model of the Bumblebee XPM missile at high subsonic speeds
- Wind-tunnel investigation at Mach numbers of 2.0 and 2.9 of several configurations of a supersonic ram-jet test vehicle
- Effect of dihedral change on the theoretical dynamic lateral response characteristics of a low-aspect-ratio straight-wing supersonic airplane
- Investigation of effect of span and spanwise location of plain and stepped spoiler ailerons on lateral control characteristics of a wing with leading edge swept back 51.3 degrees
- Factors in selecting fuels for gas-turbine powered aircraft
- Extension of boundary-layer heat-transfer theory to cooled turbine blades
- Experimental investigation of thrust augmentation of 4000-pound-thrust axial-flow-type turbojet engine by interstage injection of water-alcohol mixtures in compressor
- Experimental investigation of thrust augmentation of 4000-pound-thrust centrifugal-flow-type turbojet engine by bleedoff
- Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: effect of Reynolds number at supersonic Mach numbers on the longitudinal characteristics of a wing twisted and cambered for uniform load
- Altitude performance characteristics of tail-pipe burner with variable-area exhaust nozzle
- Altitude-wind-tunnel investigation of tail-pipe burner with converging conical burner section on J35-A-5 turbojet engine
- Effects of boundary-layer control on the longitudinal characteristics of a 45 degrees swept-forward wing-fuselage combination
- Altitude-wind-tunnel investigation of turbine performance in J47 turbojet engine
- A preliminary flight investigation of the effects of vortex generators on separation due to shock
- Longitudinal characteristics of two 47.7 degree sweptback wings with aspect ratios of 5.1 and 6.0 at Reynolds numbers up to 10 x 10(exp 6)
- Effects of leading-edge devices and trailing-edge flaps on longitudinal characteristics of two 47.7 degree sweptback wings of aspect ratios 5.1 and 6.0 at a Reynolds number of 6.0 x 10(exp 6)
- Supplementary analysis of the dynamic lateral stability characteristics of the Bell X-2 airplane as affected by variations in mass and aerodynamic parameters
- Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effect of sideslip on aerodynamic characteristics at a Mach number of 1.4 with the wing twisted and cambered
- Free-flight investigation at transonic and supersonic speeds of the rolling effectiveness of a partial-span aileron on an inversely tapered sweptback wing
- On the Formation of Shock Waves in Subsonic Flows With Local Supersonic Velocities
- Large-Scale Flight Measurements of Zero-Lift Drag at Mach Numbers from 0.90 to 1.95 of 1/14-Scale Model of the Northrop MX-775B Pilotless Aircraft with Small Body
- Investigation of frequency-response characteristics of engine speed for a typical turbine-propeller engine
- Further experiments on the flow and heat transfer in a heated turbulent air jet
- Fundamental effects of aging on creep properties of solution-treated low-carbon n-155 alloy
- Method of analysis for compressible flow through mixed-flow centrifugal impellers of arbitrary design
- Horizontal tail loads in maneuvering flight