Shock tunnel study of spiked aerodynamic bodies flying at...

Shock tunnel study of spiked aerodynamic bodies flying at hypersonic Mach numbers

Viren Menezes, S. Saravanan, K.P.J. Reddy
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Volume:
12
Language:
english
Pages:
8
DOI:
10.1007/s00193-002-0160-3
Date:
November, 2002
File:
PDF, 1.27 MB
english, 2002
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