Design And Testing Of An Axisymmetric Hypersonic Nozzle For A Low Density Wind Tunnel

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Report Number: WADC TR 56-341
Corporate Author(s): University of California
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1956-08
Pages: 95
Contract: AF 33(616)-418
DoD Project: 1363 - Wind Tunnel Studies
DoD Task: 70134
PB Number: PB125081
Identifier: AD0097178

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Provenance: IIT

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