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

An edition of Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation (1993)

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

By Lawrence D. Huebner

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Publish Date

1993

Publisher

National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,National Technical Information Service, distributor]

Language

eng

Pages

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