Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation View on Open Library

Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation

by Lawrence D. Huebner

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First published: 1993 1 language
Subjects
Aerodynamics, Hypersonic Hypersonic Aerodynamics Hypersonic wind tunnels Supersonic combustion ramjet engines

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