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 /


Autoria(s): Sehra, Arun K.
Data(s)

02/11/1979

Resumo

"AFAPL-TR-79-2010."

Cover title.

Bibliography: p. 99-102.

Mode of access: Internet.

Formato

bib

Identificador

http://hdl.handle.net/2027/coo.31924004314559

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