Effect of transpiration cooling on nozzle heat transfer
Author:
Affiliation:
1. U.S. Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio 45433-7755
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26784
Reference19 articles.
1. 4Lee, K. P. "Viscous-Shock-Layer Analysis of Hypersonic Flows Over Slender Vehicles," Ph.D. Thesis,Dept. of Mechanical Engineering and Mechanics, Old DominionUniv., Norfolk, VA,Aug. 1988.
2. Enhancements to viscous-shock-layer technique
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