Boundary layer and wake modifications to compressor design systems : the effect of blade-to-blade flow variations on the mean flow field of a transonic rotor : final report, 01 September 1976-31 August 1978 /
Data(s) |
02/11/1979
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Resumo |
"AFAPL-TR-79-2010." Cover title. Bibliography: p. 99-102. 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 Systems Command, |
Direitos |
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Palavras-Chave | #Wakes (Aerodynamics) #Boundary layer |
Tipo |
text |