Comparing Experiment and Computation of Hypersonic Laminar Boundary Layers with Isolated Roughness
Author:
Affiliation:
1. NASA Langley Research Center
2. University of Minnesota, Minneapolis
3. University of Calgary
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0236
Reference39 articles.
1. Schneider, S.P.Effects of Roughness on Hypersonic Boundary-Layer Transition,‖ Journal of Spacecraft and Rockets, 45(2), pp.193-209, March - April, 2008.
2. Smith, A.M.O., and Clutter, D.W.The Smallest Height of Roughness Capable of Affecting Boundary-Layer Transition,‖ Journal of Aerospace Sciences, 26(4), pp.229-245, April, 1959.
3. Van Driest, E.R., and McCauley, W.D.The Effect of Controlled Three-Dimensional Roughness on Boundary-Layer Transition at Supersonic Speeds,‖ Journal of Aerospace Sciences, 27(4), pp.261-271, April, 1960.
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