Measurement of Heat Transfer Rate on Backward-Facing Steps at Hypersonic Mach Number
Author:
Affiliation:
1. Airbus Engineering Centre India Pvt. Ltd., Bangalore 560 016, India
2. Indian Institute of Science, Bangalore 560 012, India
3. University of New South Wales, Canberra ACT 2600, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.47101
Reference21 articles.
1. The reattachment and relaxation of a turbulent shear layer
2. Hayne, M. J. "Hypervelocity Flow over a Rearward Facing Steps," Ph.D. Thesis,Univ. of Queensland, Brisbane, Australia, 2004.
3. Laminar heat transfer to a two-dimensional backward facing step from the high-enthalpy supersonic flow in the shock tube
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