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
Miscellaneous
No indication
English
Controlled recovery of nonlifting satellites
Engineering Index Backfile | 1960
|Supersonic wave drag of nonlifting Delta wings with linearly varying thickness ratio
Engineering Index Backfile | 1952
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