Flow Separation and Heat Transfer in High Area Ratio Nozzles

Author:

Hagemann Gerald1,Preuss A.1,Grauer F.1,Frey M.1,Kretschmer J.1,Ryden R.2

Affiliation:

1. EADS Space Transportation GmbH

2. Volvo Aero Corporation

Publisher

American Institute of Aeronautics and Astronautics

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Active Control of Dual-Bell Nozzle Operation Mode Transition by Film Cooling and Mixture Ratio Variation;Journal of Propulsion and Power;2020-01

2. Hot Flow Testing of Dual Bell Nozzles;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

3. Shock pattern in the plume of rocket nozzles - needs for design consideration;Shock Waves;2009

4. Shock pattern in the plume of rocket nozzles: needs for design consideration;Shock Waves;2008-04-01

5. The V2+ Nozzle Extension Demo: A milestone on the route to sandwich nozzle production.;57th International Astronautical Congress;2006-10-02

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