Pressure gradient effects on supersonic boundary layer turbulence : final report /
| Data(s) |
04/02/1979
|
|---|---|
| Resumo |
"Carried out by the Fluid Mechanics Section of the Aeronutronic Division of the Ford Aerospace & Communications Corporation." "AFFDL-TR-3005." Cover title. Bibliography: p. 165-167. Mode of access: Internet. |
| Formato |
bib |
| Identificador | |
| Idioma(s) |
eng |
| Publicador |
Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, 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 | #Aerodynamics, Supersonic #Turbulent boundary layer |
| Tipo |
text |
