Transpiration Cooling with Supersonic Flows and Foreign Gas Injection
Author:
Publisher
American Institute of Aeronautics and Astronautics
Reference39 articles.
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1. Lateral Wall Temperature Effects in a Transpiration Cooled Scramjet Model Combustor with Shock-Boundary Layer Interaction;AIAA Propulsion and Energy 2021 Forum;2021-07-28
2. Research progress on active thermal protection for hypersonic vehicles;Progress in Aerospace Sciences;2020-11
3. Lateral Wall Pressure Effects in a Transpiration Cooled Scramjet Model Combustor with Shock-Boundary Layer Interaction;AIAA Propulsion and Energy 2020 Forum;2020-08-17
4. Large-eddy simulation of transpiration cooling in turbulent channel with porous wall;Applied Thermal Engineering;2018-12
5. Numerical Modeling of Transpiration-Cooled Turbulent Channel Flow with Comparisons to Experimental Data;Journal of Thermophysics and Heat Transfer;2018-07
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