Flow field approximation for sonic boom shock wave generation by thin nonlifting rectangular wing
Uniform approximations for shocks generated by thin nonlifting rectangular wings
01.01.1971
Sonstige
Keine Angabe
Englisch
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
|