Chun-lin GONG  , Bing CHEN  , Jian-lei WANG  , Tian-gang LI  , Liang-xian GU  , Shuo TANG

DOI Number XXX-YYY-ZZZ

Conference Number HiSST 2018_41701142

The Rocket-based combined cycle (RBCC) engine is effective propulsion for the launch vehicle, but it will produce complex design problems, especially for the airframe-propulsion integration. This paper is mainly on the research on wind tunnel test and test method. The test relationship is established to obtain the performance of the airframe-propulsion integration. The test results are corrected by CFD. The scaling effect and the correction of flight test and ground test are also discussed in this research. The relationship of components’ test and integrated test is cleared, and the corrected method will establish the database of the launch vehicle’s performance, which can be used to direct the design of such vehicle. The specific works will be given in the full text.

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In Categories: Advanced Airframe Materials, HiSST 2018, Hypersonic Aerodynamics, Hypersonic Propulsion, Propulsion Systems and Components, Testing and Evaluation
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