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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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Wind tunnel aerodynamic characteristics of subsonic nuclear powered canard aircraft model
Wind tunnel investigation of aerodynamic characteristics of cone-cylinder-flare multistage missile configurations at supersonic speed
Aerodynamic characteristics of canard configuration at subsonic and supersonic speeds with deflected wing tips for longitudinal and directional stability
Effect of forebody strakes on aerodynamic characteristics in sideslip and pitch of hypersonic aircraft configurations
Effects of aspect ratio and canopy shape on longitudinal and lateral aerodynamic characteristics of parawings having 50 degree sweepback leading edges
Parametric study of Newtonian aerodynamic characteristics of right elliptical raked-off cones for cone thickness ratios
Wind tunnel test program for study of aerodynamic characteristics of T-tail aircraft at high angles of attack
Flight characteristics of large jet transports with powered-lift systems
Effect of rearward body strakes on transonic aerodynamic characteristics of unswept-wing fighter aircraft
Wind tunnel testing to determine effects of wing planform modifications on longitudinal aerodynamic characteristics of variable-sweep M planform wing
Longitudinal stability and control characteristic of M wing aircraft at various Mach numbers
Consistent field Monte Carlo method calculation for collision effect on electron-ion diode characteristics and for hard sphere electron- neutral collision effect for monoenergetic- thermionic emission
Intermediate thrust sub-arcs analyzed by method of characteristic constants for optimum retrothrust program in inverse-square-law force field
Magnetic annular arc thrust and current-voltage characteristics, using various working fluids
Numerical method to obtain pressure distribution on arbitrary wing planform of various surface shapes with attention to aerodynamic characteristics
Aerodynamic characteristics of spherically blunted cones at Mach numbers from 0.5 to 5.0
Static and propulsive performance characteristics of ducted fan at zero angle of attack for several fan blade angles
Effects of wing planform on aerodynamic characteristics in pitch and sideslip of wing-body-tail model at supersonic wind tunnel speeds