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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Effect of body cross sections and width-height ratio on performance of bodies and delta-wing- body combinations at Mach 6.9
Effect of thickness and sweep angle on longitudinal aerodynamic characteristics of slab delta planforms at hypersonic speed
Longitudinal aerodynamic characteristics at transonic speeds of V/STOL aircraft configuration with fixed delta wing having auxiliary variable sweep outboard panels
Low speed measurements of oscillatory lateral stability derivatives of 60 degree delta wing bomber model
Pressure distributions on flat plate delta wing swept 65 deg at hypersonic speeds at angles of attack from 65 deg to 115 deg and angles of roll from 0 deg to 25 deg at 90 deg angle of attack
Aerodynamic characteristics of thick delta wings at subsonic to supersonic speeds and angles of attack to 50 deg
Hypersonic pressure and heat transfer tests on delta wings with laminar and turbulent boundary layers
Wind tunnel stability test of low aspect ratio delta winged model equipped with sharp-edged strakes
Heat-transfer and pressure distributions on 60 and 70 deg swept delta wings with turbulent boundary layers
Vortex lift calculation for sharp-edge delta wings based on leading edge suction analogy
Bursting of conical vortex sheet above delta wing surface at low speeds
Hypersonic flight performance of basic and modified delta wings with diamond cross sections
Launch window, trajectory shaping, and lunar orbit mission analyses for improved Delta launch vehicle and advanced IMP-D spacecraft
In-flight performance of solid propellant rocket engine for Delta launch vehicle
Acoustic noise measurements during launching of improved Delta, TAT/Agena-D, and Atlas Agena-D launch vehicles
Constant chord, trailing edge, control deflection effects on aerodynamic loading characteristics of 60 degree delta wing-body combination at transonic speeds
Large scale low speed wind tunnel tests of delta winged supersonic transport model to determine aerodynamic effects of forward and reverse thrust