Investigation of small surface protuberances upstream of turbulent boundary layer separation produced by a skewed shock wave at Mach 3 /
| Data(s) |
01/01/1976
|
|---|---|
| Resumo |
"Interim report for period January 1976-February 1976." Cover title. Bibliography: p. 5. Mode of access: Internet. |
| Formato |
bib |
| Identificador | |
| Idioma(s) |
eng |
| Publicador |
Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Syspems 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 | #Shock waves #Aerodynamics, Supersonic #Turbulent boundary layer |
| Tipo |
text |
