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Numerical study of shock/boundary layer interaction in supersonic overexpanded nozzles

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https://hal.archives-ouvertes.fr/hal-02082612
Contributor : Abdellah Hadjadj Connect in order to contact the contributor
Submitted on : Thursday, March 28, 2019 - 12:39:01 PM
Last modification on : Tuesday, October 19, 2021 - 4:14:19 PM

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Abdellah Hadjadj, Y. Perrot, S. Verma. Numerical study of shock/boundary layer interaction in supersonic overexpanded nozzles. Aerospace Science and Technology, Elsevier, 2015, 42, pp.158-168. ⟨10.1016/j.ast.2015.01.010⟩. ⟨hal-02082612⟩

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