Numerical Analysis on Detonation Tube for Simulating the Rocket Exhaust Gas at High Enthalpy Shock Tunnel
16th, AIAA International Space Planes and Hypersonic Systems and Technologies Conference ; 2009 ; Bremen, Germany
2009-01-01
7 pages
Includes bibliographic references and index
Conference paper
English
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Detonation tube technique for simulating rocket plumes in space environment
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