Effect of Coolant Inlet Conditions on Supersonic Film Cooling
Author:
Affiliation:
1. Department of Thermal Engineering, Tsinghua University, 100084 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33268
Reference15 articles.
1. also AIAA Paper 1994-2757, 1994. doi:10.2514/6.1994-2757
2. Surface cooling of scramjet engine inlets using heat pipe, transpiration, and film cooling
3. Effects of hydrogen active cooling on scramjet engine performance
4. Film cooling with air and helium injection through a rearward-facingslot into a supersonic air flow.
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