Unsteady Transition From a Mach to a Regular Shockwave Intersection
Author:
Affiliation:
1. Department of Chemical Engineering, Computational Fluid Dynamics Unit National Technical University of Athens (N.T.U.A.) 9, Heroon Polytechniou str., Zografou, GR-15780, GREECE
Abstract
Publisher
World Scientific and Engineering Academy and Society (WSEAS)
Subject
General Physics and Astronomy
Reference29 articles.
1. K.Naidoo and B.W.Skews, Dynamic transition from Mach to regular reflection of shock waves in a steady flow, J. Of Fluid Mechanics, vol.750,385-400, July 2014.
2. M.K.Hryniewicki, J.Gottlieb, C.Groth, Transition boundary between regular and Mach reflections for a moving shock interacting with a wedge in inviscid and polytropic air, Shock Waves 27,523-550, 2017.
3. J.Gottlieb, M.K. Hryniewicki, C.Groth,Transition boundary between regular and Mach reflections for a moving shock interacting with a wedge in inviscid and polytropic argon, Shock Waves 29, 795-816, 2019.
4. J.D. Anderson, Supersonic and High Temperature Gas Dynamics, McGraw-Hill, 1989.
5. Chapman CJ. High Speed Flow, Cambridge Univ. Press (Cambridge Texts in Applied Mathematics, 23), Cambridge, 2000.
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