Skin friction, heat transfer, and pressure measurements on hypersonic inlet compression surfaces in the Mach number range 7.5 to 16.
| Data(s) |
31/12/1969
|
|---|---|
| Resumo |
Cornell Aeronautical Laboratory, Inc., Buffalo. Report no. AA-1948-Y-3 Mode of access: Internet. |
| Formato |
bib |
| Identificador | |
| Idioma(s) |
eng |
| Publicador |
[Wright-Patterson Air Force Base, Ohio, Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, |
| 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 | #Boundary layer. #Heat #Skin friction (Aerodynamics) #Aerodynamics, Hypersonic. |
| Tipo |
text |
