Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Aerospace Engineering,Nuclear Energy and Engineering,General Chemical Engineering
Reference29 articles.
1. Laminar heat transfer to a two-dimensional backward facing step from the high enthalpy supersonic flow in the shock tube;Rom;AIAA J.,1964
2. Measurement of heat transfer rate on backward facing steps at hypersonic Mach number;Reddeppa;J. Thermophys. Heat Transf.,2011
3. Hypersonic turbulent boundary-layer interference heat transfer in vicinity of protuberances;Truitt;AIAA J.,1965
4. P.B. Burbank, R.A. Newlander, I.K. Collins, 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.
5. Aerodynamic heating characteristics over a protuberance in hypersonic flows using fast response thermo gauges;Lee;Int. J. Aeronaut. Space Sci.,2010
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