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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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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
Wind tunnel stability tests of pinch of modified half ring wing body and swept wing body combinations at supersonic speeds
Simulated wing damage effects on aerodynamic characteristics of swept-wing airplane model
Wind tunnel investigation of tip vortex structure of semispan wing for several wing-tip modifications
Wind tunnel tests to determine effects of wing dihedral angle on aerodynamic characteristics of highly swept fixed-wing configuration
Second order slender wing theory for calculating supersonic flow over low aspect ratio wings with subsonic leading edges and leading edge separation
Trisonic wind tunnel static stability tests on straight wing and delta wing space shuttle models