Laminar boundary layer stability calculation for contoured Mach 6 nozzle
Author:
Publisher
Pleiades Publishing Ltd
Subject
Nuclear and High Energy Physics,Radiation
Link
https://link.springer.com/content/pdf/10.1134/S0869864320010035.pdf
Reference20 articles.
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3. J. Hofferth, R. Bowersox, and W. Saric, The Mach 6 quiet tunnel at Texas A&M: quiet flow performance, in: 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conferences, Fluid Dynamics and Co-located Conf., AIAA Paper, 2010, No. 2010–4794.
4. C.-H. Zhang, Q. Tang, and C.-B. Lee, Hypersonic boundary-layer transition on a flared cone, Acta Mechanica Sinica, 2013, Vol. 29, No. 1, P. 48–54.
5. D. Gang, S. Yi, and X. Lu, Design and performance of a hypersonic quiet wind tunnel at NUDT, in: 21st AIAA Int. Space Planes and Hypersonics Technologies Conf., AIAA Paper, 2017, No. 2017–2305.
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