Transitional Behavior of Dual Bell Nozzles: Contour Optimization
Author:
Affiliation:
1. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-3841
Reference13 articles.
1. A critical assessment of dual-bell nozzles
2. Propulsion and Flight Performance Evaluation of Dual-Bell Nozzles
3. Numerical Parametric Analysis of Dual-Bell Nozzle Flows
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2. Rocket nozzles: 75 years of research and development;Sādhanā;2021-04-11
3. Active Control of Dual-Bell Nozzle Operation Mode Transition by Film Cooling and Mixture Ratio Variation;Journal of Propulsion and Power;2020-01
4. Numerical Model for Nozzle Flow Application Under Liquid Oxygen/Methane Hot-Flow Conditions;Journal of Propulsion and Power;2018-01
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