Boundary-Layer Transition on a Hypersonic Forebody: Experiments and Calculations
Author:
Affiliation:
1. Centre National de la Recherche Scientifique, 45071 Orléans Cedex 2, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.51570
Reference24 articles.
1. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition
2. Ground Test Studies of the HIFiRE-1 Transition Experiment Part 1: Experimental Results
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