The shock layer concept and three-dimensional hypersonic boundary layers.
| Data(s) |
28/12/1961
|
|---|---|
| Resumo |
"This report is based on research sponsored by the U.S. Navy through the Office of Naval Research, Contract Nonr-2653(00)" Mode of access: Internet. |
| Formato |
ren |
| Identificador | |
| Idioma(s) |
eng |
| Publicador |
Buffalo, Cornell Aeronautical Laboratory, |
| 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 | #Aerodynamics, Hypersonic. #Shock waves. #Boundary layer. |
| Tipo |
text |
