Analysis of the Oscillatory Flows of Multiple Shock Waves in a Constant Area Duct
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Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s11630-024-1968-2.pdf
Reference39 articles.
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3. Wagner J.L., Yuceil K.B., Valdivia A., Clemens N.T., Dolling D.S., Experimental investigation of unstart in an inlet/isolator model in Mach 5 flow. AIAA Journal, 2009, 47(6): 1528–1542.
4. Su W.Y., Zhang K.Y., Back-pressure effects on the hypersonic inlet-isolator pseudo shock motions. Journal of Propulsion and Power, 2013, 29(6): 1391–1399.
5. Klomparens R.L., Driscoll J.F., Gamba M., Response of a shock train to downstream back pressure forcing. 54th AIAA Aerospace Sciences Meeting, San Diego, California, USA, 2016, Paper No. AIAA 2016-0078.
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