Flow field approximation for sonic boom shock wave generation by thin nonlifting rectangular wing
Uniform approximations for shocks generated by thin nonlifting rectangular wings
1971-01-01
Sonstige
Keine Angabe
Englisch
Supersonic wave drag of nonlifting Delta wings with linearly varying thickness ratio
Engineering Index Backfile | 1952
|Laminar Separated Flow Nonlifting Ellipses
AIAA | 1975
|Engineering Index Backfile | 1947
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