SEARCH · Engineering Papers
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Static longitudinal stability characteristics of blunted glider reentry configuration
Performance and static stability of supersonic aircraft configuration with lift interference
Pressure distributions over forward portion of project fire space-vehicle configuration at subsonic speed
Water landings of winged reentry configuration having outboard folding wing panels - models used
Free flying 1/3-scale model of a lifting reentry configuration and low subsonic stability and control characteristics
Static longitudinal stability and control characteristics of air-to-surface canard missile configuration in transonic range
Aerodynamic and control studies of lifting reentry configurations at angles of attack up to 90-deg at supersonic speeds
Static stability and control characteristics of manned lenticular reentry configuration at low subsonic speeds
Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90-degrees
Aerodynamics of disk reentry configurations, for manned space flight, with elliptic cross sections and thickness diameter ratios of 0.225 and 0.325
Low speed wind tunnel analysis of annular-jet configuration in ground range
High altitude base heating of 4-engine rocket nozzle configuration
Wind-tunnel investigation of longitudinal and lateral aerodynamic characteristics of hypersonic glider with several booster configurations
Heat transfer and pressure distribution over reentry configuration for five-stage scout vehicle
Aerodynamic characteristics of variable-wing-sweep configuration with spoiler-slot-deflector control system & swept back outer wing panels
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configurations
Skin temperature and surface pressure of blunted cone-cylinder-flare configuration free flight test vehicle to hypersonic speeds