Transitional shockwave/boundary layer interaction experiments in the R2Ch blowdown wind tunnel
Author:
Publisher
Springer Science and Business Media LLC
Subject
Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics
Link
https://link.springer.com/content/pdf/10.1007/s00348-022-03395-9.pdf
Reference52 articles.
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2. Aymer De La Chevalerie D, Fonteneau A, De Luca L, Cardone G (1997) Görtier-type vortices in hypersonic flows: The ramp problem. Exp Thermal Fluid Sci 15(2 SPEC. ISS.):69–81. https://doi.org/10.1016/s0894-1777(97)00051-4
3. Benay R, Chanetz B, Mangin B, Vandomme L, Perraud J (2006) Shock wave/transitional boundary-layer interactions in hypersonic flow. AIAA J 44(6):1243–1254. https://doi.org/10.2514/1.10512
4. Benitez EK, Jewell JS, Schneider SP, Esquieu S (2020) Instability measurements on an axisymmetric separation bubble at mach 6. In: Aiaa aviation 2020 forum, vol 1 PartF, pp 1–29. https://doi.org/10.2514/6.2020-3072
5. Benitez EK, Jewell JS, Schneider SP (2021) Separation bubble variation due to small angles of attack for an axisymmetric model at mach 6. In: AIAA Scitech 2021 Forum, pp 1–23. https://doi.org/10.2514/6.2021-0245
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