Numerical investigation of shock train unsteady movement in a mixing duct

Author:

Lu Lei,Wang Yi,Fan Xiao-qiang,Yan Guo-wei,Pan Jing-wen

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference25 articles.

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3. Equivalence ratio and constriction effects on RBCC thrust augmentation;Koupriyanov;Acta Astronaut.,2011

4. Millisecond-scale shock-train evolution in high-pressure ratio nozzles: schlieren imaging and qualitative analysis of shock-boundary layer interaction;Keanini;Proc. Inst. Mech. Eng., G J. Aerosp. Eng.,2014

5. Fifty years of shock-wave/boundary-layer interaction research: what next;Dolling;AIAA J.,2012

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