Publisher
Cambridge University Press (CUP)
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Reference109 articles.
1. van Ingen, J. L. 1956 A suggested semi-empirical method for the calculation of the boundary layer transition region. Tech. Rep. VTH-74. Technische Hogeschool Delft, Vliegtuigbouwkunde.
2. Hornung, H. G. 1992 Performance data of the new free-piston shock tunnel at GALCIT. In AIAA/ASME/SAE/ASEE 28th Joint Propulsion Conference and Exhibit, 1992, AIAA paper 92-3943.
3. Significant supersonic modes and the wall temperature effect in hypersonic boundary layers;Knisely;AIAA J.,2019
4. Wheaton, B. M. , Berridge, D. C. , Wolf, T. D. , Stevens, R. T. & McGrath, B. E. 2018 Boundary Layer Transition (BOLT) flight experiment overview. AIAA Paper 2018-2892.
5. Johnson, H. B. & Candler, G. V. 2005 Hypersonic boundary layer stability analysis using PSE-Chem. AIAA Paper 2005-5023.
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