Comparative Analysis of Turbulence Models for Turbulent Non-premixed Combustion: A Hybrid Rocket Engine Case Study
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Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-67241-5_14
Reference26 articles.
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3. Marxman, G., Gilbert, M.: Turbulent boundary layer combustion in the hybrid rocket. Symposium (International) on Combustion, 9(1), 371–383 (1963)
4. Marxman, G.A.: Combustion in the turbulent boundary layer on a vaporizing surface. Symposium (International) on Combustion, 10(1), 1337–1349 (1965)
5. Majdalani, J., Vyas, A.: Inviscid models of the classic hybrid rocket. In: 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics (2004)
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