Active Control of Dual-Bell Nozzle Operation Mode Transition by Film Cooling and Mixture Ratio Variation
Author:
Affiliation:
1. DLR, German Aerospace Center, D-74239 Lampoldshausen, Germany
2. RWTH Aachen University, D–52062 Aachen, Germany
Funder
Deutsches Zentrum für Luft- und Raumfahrt
Deutsche Forschungsgemeinschaft
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Reference59 articles.
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4. GéninC. “Experimental Study of Flow Behaviour and Thermal Loads in Dual Bell Nozzles,” Ph.D. Thesis, Univ. of Valenciennes and Hainaut-Cambrésis, Famars, France, 2010.
5. Ariane 5 Performance Optimization Using Dual-Bell Nozzle Extension
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