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1950-1959 (4,118)
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Performance of a Single Fuel-vaporizing Combustor With Six Injectors Adapted for Gaseous Hydrogen
Some Research on the Lift and Stability of Wing-Body Combinations
Preliminary analysis of hydrogen-rich hypersonic ramjet operation
An analytical evaluation of the effects of an aerodynamic modification and of stability augmenters on the pitch behavior and probable pilot opinion of two current fighter airplanes
Effects of components and various modifications on the drag and the static stability and control characteristics of a 42 deg swept-wing fighter-airplane model at Mach numbers of 1.60 to 2.50
Combustor performance with various hydrogen-oxygen injection methods in a 200-pound-thrust rocket engine
Off-Design Performance of Divergent Ejectors
Off-design performance of divergent ejectors
Rocket-model investigation to determine the lift and pitching effectiveness of small pulse rockets exhausted from the fuselage over the surface of an adjacent wing at Mach numbers from 0.9 to 1.8
Screaming tendency of the gaseous-hydrogen - liquid-oxygen propellant combination
Use of highly reactive chemical additives to improve afterburner performance at altitude
Use of highly reactive chemical additives to improve afterburner performance at altitude
Some notes on the probable damage to an intercontinental-ballistic-missile warhead following puncture of the heat shield
Analysis of pressure data obtained at transonic speeds on a thin low-aspect-ratio cambered delta wing-body combination
Heat Transfer Measured in Free Flight on a Slightly Blunted 25 deg Cone-Cylinder-Flare Configuration at Mach Numbers up to 9.89
Large-scale wind-tunnel tests of a jet-transport-type model with leading- and trailing-edge high-lift devices
Static and dynamic-rotary stability derivatives of an airplane model with an unswept wing and a high horizontal tail at Mach numbers of 2.5, 3.0, and 3.5
Effect of spike-tip and cowl-lip blunting on inlet performance of a Mach 3.0 external-compression inlet
Effect of spike-tip and cowl-lip blunting on inlet performance of a Mach 3.0 external- compression inlet
Experimental investigation of effect of spike- tip and cowl-lip blunting on the internal performance of a two-cone cylindrical-cowl inlet at mach number 4.95
Experimental Study of Ballistic-Missile Base Heating with Operating Rocket
Investigation of Inlet Control Parameters for an External-Internal-Compression Inlet from Mach 2.1 to 3.0
A Flight Study of the Effects of Noise Filtering in the Attack Display on the Pilot's Tracking Performance
Aerodynamic performance and static stability and control of flat-top hypersonic gliders at Mach numbers from 0.6 to 18
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