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Feasibility study of high-temperature synthetic-air heater for use with a mach 8 to 9 hypersonic tunnel. :

Lezberg, Erwin A.

Feasibility study of high-temperature synthetic-air heater for use with a mach 8 to 9 hypersonic tunnel. : - - Washington, D.C. NASA 1965 - 19 - NBS : SMT : SP : 400 - 27 - 1974 .

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Universal Decimal Class. No.: LNASA TN D-2878

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