Affiliation:
1. von Kármán Institute for Fluid Dynamics
Publisher
American Institute of Aeronautics and Astronautics
Reference65 articles.
1. Characterization of hypersonic roughness-induced boundary-layer transition
2. 4Masutti, D., Ground testing investigation of hypersonic transition phenomenon for a re-entry vehicle, Ph.D. thesis, Technische Universiteit Delft - vonKarman Institute for Fluid Dynamics, 2013.
Cited by
15 articles.
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