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High Enthalpy Wind Tunnel Tests of Three-Dimensional Section Controllable Internal Waverider Hypersonic Inlet

  • Published:2009-01-05 Issue: Volume: Page:
  • ISSN:
  • Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
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Author:

You Yancheng1,Liang Dewang1,Guo Rongwei1

Affiliation:

1. Nanjing University of Aeronautics and Astronautics

Publisher

American Institute of Aeronautics and Astronautics

Reference24 articles.

1. M.A.Lewis,"HypersonicPropulsionAirframeIntegrationOverview,"AIAA2003-4405,2003.

2. F. J. Malo, D. V. Gaitonde, "Analysis of an Innovative Inward Turning Inlet Using an Air-JP8 Combustion MixtureatMach7,"AIAA2006-3041,2006.

3. F. J. Malo, D. V. Gaitonde, "Numerical Investigation of an Innovative Inward Turning Inlet," AIAA 2005-4871,2005.

4. Inverse Waverider Design for Inward Turning Inlets

5. A. P. Kothari, C. Tarpley, T. A. McLaughlin, B. S. Babu, J. W. Livingston, "Hypersonic Vehicle Design UsingInwardTurningFlowFields,"AIAA1996-2552,1996.

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