Wind tunnel tests for separation dynamics modeling of a two-stage hypersonic vehicle
10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference ; 2001 ; Kyoto , Japan
01.01.2001
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Wind Tunnel Tests for Separation Dynamics Modeling of a Two-Stage Hypersonic Vehicle
British Library Conference Proceedings | 2001
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