SEARCH · Search NASA
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.
Aerodynamic characteristics in pitch of several wing-body combinations with wedge-shaped planform located above and below a swept delta wing
Effects of airfoil section shape and thickness on supersonic performance characteristics of wing body configuration employing warped highly swept arrow wing
Effects of wing planform on aerodynamic characteristics in pitch and sideslip of wing-body-tail model at supersonic wind tunnel speeds
Wing-tip droop effects on performance and stability of canard delta-wing aircraft at supersonic speeds
Skewed wing tip control effects on variable sweep wing-fuselage configuration
Wing pivot location effect on longitudinal aerodynamic characteristics of variable sweep wing having M planform
Free flight tests of 45-deg swept wings of 3.15 aspect ratio and 0.54 taper ratio to measure wing damping and possible transonic flutter
Low-speed longitudinal static stability & control characteristics of aircraft with swept wings & tail surfaces outboard of wing tips
Stability and control of variable sweep wing configuration with outboard wing panels swept back 75 degrees at Mach 2.01
Wing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Mach 2.01
Wind tunnel testing to determine effects of wing planform modifications on longitudinal aerodynamic characteristics of variable-sweep M planform wing
Effect of wing leading-edge shape on aerodynamic characteristics of 67 deg swept wing-body model at Mach 1.50 to 4.63
Numerical procedure for analyzing and designing wings and wing-body combinations in supersonic flow
Wing-body combinations with wings of very low aspect ratio at supersonic speeds
Horizontal-tail height, wing height, and dihedral effects on longitudinal and lateral stability characteristics of 76 deg swept arrow wing aircraft model
An investigation has been conducted in the Langley 300 MPH 7- by 10-foot tunnel to determine the effect of negative dihedral, tip droop, and wing-tip shape on the low-speed aerodynamic characteristics of a complete model having a 45 degrees sweptback wing. Longitudinal and lateral stability characteristics were obtained for the model with and without tail surfaces.
This lecture concerns the combining effects in airplane wings so as to save some of the dead weight.
Tabulation of wind tunnel pressure data and section aerodynamic characteristics for a reflex cambered wing