Method permits analysis of noncircular bodies and calculation of wing-body interference effects in presence of body closure, two features not previously available. In addition, use of vortex distribution, having linear variation in streamwise direction, results in improved chordwise pressure distributions on wing and tail surfaces.
Improved method for aerodynamic analysis of wing-body-tail configurations in subsonic and supersonic flow
01.03.1974
Sonstige
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Englisch
Aerodynamic Optimization of Subsonic Flying Wing Configurations
British Library Conference Proceedings | 2002
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