Hypersonic Interference Heating on Flat Plate with Short Three-Dimensional Protuberances
Author:
Affiliation:
1. Department of Aerospace Engineering, Indian Institute of Science, Bangalore, Karnataka 560 012, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052658
Reference24 articles.
1. NestlerD. “The Effects of Surface Discontinuities on Convective Heat Transfer in Hypersonic Flow,” AIAA Paper 1985-0971, 1985.
2. BurbankP. B.NewlanderR. A.CollinsI. K. “Heat-Transfer and Pressure Measurements on a Flat-Plate Surface and Heat-Transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51 and 4.44,” NASA TN-D-1732, 1962.
3. Hypersonic turbulent boundary-layer interference heat transfer in vicinity of protuberances
4. A Survey of the Effects of Small Protuberances on Boundary-Layer Flows
5. Three-dimensional protuberance interference heating in high speed flow
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