Film Cooling of a Blunt Body in a Supersonic High-Enthalpy Flow
Author:
Affiliation:
1. Elbit Systems, Ltd., 47100 Ramat Hasharon, Israel
2. ORT Braude Academic College of Engineering, 2161002 Karmiel, Israel
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.A34865
Reference20 articles.
1. Investigation of Transpiration Cooling Effectiveness for Air- Breathing Hypersonic Vehicles
2. Qualification of Active Cooling Concepts in Ground Facilities
3. GülhanA.EsserB. “Arc-Heated Facilities as a Tool to Study Aerothermodynamic Problems of Reentry Vehicles,” Advanced Hypersonic Test Facilities, edited by LuF.MarrenD., Vol. 198, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2002, pp. 375–403. 10.2514/5.9781600866678.0375.0403
4. The flow of a jet from a body opposing a supersonic free stream
5. StalderJ.R.InouyeM. “A Method of Reducing Heat Transfer to Blunt Bodies by Air Injection,” NACA RM A56B27a, May 1956.
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