On the use of impact theory for slender configurations exhibiting flow separation /
| Data(s) |
05/02/1963
|
|---|---|
| Resumo |
Photocopy. "Prepared for Air Programs, Office of Naval Research [under] Contract no. Nonr-3103(00). Vidya Project no. 26/C." Bibliography: leaves 16-17 (1st set) Mode of access: Internet. |
| Formato |
ren |
| Identificador | |
| Idioma(s) |
eng |
| Publicador |
Palo Alto, Calif. : Vidya, a division of Itek Corp., |
| Direitos |
Items in this record are available as Public Domain, Google-digitized. View access and use profile at http://www.hathitrust.org/access_use#pd-google. Please see individual items for rights and use statements. |
| Palavras-Chave | #Drag (Aerodynamics) #Aerodynamics, Supersonic |
| Tipo |
text |
