Affiliation:
1. Indian Institute of Technology Guwahati
Publisher
American Institute of Aeronautics and Astronautics
Reference24 articles.
1. SHOCK-INDUCED BOUNDARY LAYER SEPARATION IN OVER-EXPANDED CONICAL EXHAUST NOZZLES
2. Numerical simulation of transient flows in a rocket propulsion nozzle
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4. Origin of flow asymmetry in planar nozzles with separation