Numerical study of shock/boundary layer interaction in supersonic overexpanded nozzles - Archive ouverte HAL Access content directly
Journal Articles Aerospace Science and Technology Year : 2015
No file

Dates and versions

hal-02082612 , version 1 (28-03-2019)

Identifiers

Cite

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

Altmetric

Share

Gmail Facebook X LinkedIn More