Experimental study and analysis of shock train self-excited oscillation in an isolator with background waves
Author:
Funder
National Natural Science Foundation of China
Publisher
Zhejiang University Press
Subject
General Engineering
Link
https://link.springer.com/content/pdf/10.1631/jzus.A2000042.pdf
Reference38 articles.
1. Cai JH, Zhou J, Liu SJ, et al., 2017. Effects of dynamic backpressure on shock train motions in straight isolator. Acta Astronautica, 141:237–247. https://doi.org/10.1016/j.actaastro.2017.10.013
2. Carroll BF, Dutton JC, 1990. Characteristics of multiple shock wave/turbulent boundary-layer interactions in rectangular ducts. Journal of Propulsion and Power, 6(2):186–193. https://doi.org/10.2514/3.23243
3. Fiévet R, Koo H, Raman V, et al., 2017. Numerical investigation of shock-train response to inflow boundary-layer variations. AIAA Journal, 55(9):2888–2901. https://doi.org/10.2514/1.J055333
4. Geerts JS, Yu KH, 2016. Shock train/boundary-layer interaction in rectangular isolators. AIAA Journal, 54(11):3450–3464. https://doi.org/10.2514/1.J054917
5. Gnani F, Zare-Behtash H, Kontis K, 2016. Pseudo-shock waves and their interactions in high-speed intakes. Progress in Aerospace Sciences, 82:36–56. https://doi.org/10.1016/j.paerosci.2016.02.001
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