Experimental Study of Supersonic Laminar Base Flow with and without Suction
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50668
Reference24 articles.
1. Laminar heat transfer to a two-dimensional backward facing step from the high-enthalpy supersonic flow in the shock tube
2. Hypersonic boundary-layer separation and the base flow problem.
3. A new theoretical solution of the laminar, hypersonic near wake.
4. An experimental study of supersonic flow over a rearward facing step.
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2. Computational Analysis of a Rarefied Hypersonic Flow over Backward-Facing Steps;Journal of Thermophysics and Heat Transfer;2019-07
3. Flow Behind a Step in High-Enthalpy Laminar Hypersonic Flow;AIAA Journal;2010-07
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