A study of the overall problems of the true-temperature, hypersonic wind tunnel having semi-continuous operation and the preferred methods of solution.


Autoria(s): Palmer, George M.
Data(s)

31/12/1969

Resumo

"Supported by the McDonnell Aircraft Corporation under Contract no. 6140-20 P. O. 7S4899-R. Purdue Research Foundation. Research project no. 1717. Project Ae-33.

Mode of access: Internet.

Formato

ren

Identificador

http://hdl.handle.net/2027/coo.31924004672162

Idioma(s)

eng

Publicador

[Lafayette, Ind., Purdue University, School of Aeronautical Engineering,

Direitos

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Palavras-Chave #Aerodynamic heating #Hypersonic wind tunnels
Tipo

text