Investigation of test time at undertailored conditions in a shock tunnel.


Autoria(s): Martin, James F.; Cornell Aeronautical Laboratory Hypersonic Research Dept.
Data(s)

31/12/1969

Resumo

Cover title.

Mode of access: Internet.

Formato

ren

Identificador

http://hdl.handle.net/2027/coo.31924004404087

Idioma(s)

eng

Publicador

Buffalo, Cornell Aeronautical Laboratory, Inc.

Direitos

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Palavras-Chave #Aerodynamics, Hypersonic #Shock tubes
Tipo

text