Shock tube test time limitation due to turbulent wall boundary layer.


Autoria(s): Aerospace Corporation.; Mirels, Harold.
Data(s)

29/09/1963

Resumo

At head of title: SSD-TDR-63-78. Report no. TDR-169 (3230-12)TR-3.

Mode of access: Internet.

Formato

ren

Identificador

http://hdl.handle.net/2027/coo.31924004403832

Idioma(s)

eng

Publicador

[El Segundo?]

Direitos

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Palavras-Chave #Boundary layer #Shock tubes
Tipo

text