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by Ming Han Tang
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Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
Thomas A. Byrdsong
High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
Robert S. Jankovsky
User's guide
Patricia A. Kerr
F-18 High Alpha Research Vehicle surface pressures
David F. Fisher
In-flight investigation of shuttle tile pressure orifice installations
Timothy R. Moes
Thomas A Byrdsong
Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations
Jacob H. Lichtenstein
A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft
Lisa J. Bjarke
Fluctuating loads measured on an over-the-wing supersonic jet model
Conrad M. Willis