The work is concerned with the disturbance region associated with a yawed hypersonic delta wing of diamond cross-section. The analysis is presented for zero angle of attack, and it is then shown how angle-of-attack effects may be included. (Author)
Pressure Distribution on a Hypersonic delta Wing of Diamond Cross-Section
1967
13 pages
Report
Keine Angabe
Englisch
Delta wing shock shape at hypersonic speed
AIAA | 1971
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British Library Conference Proceedings | 1993
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