Author:
Zubin M. A.,Maksimov F. A.,Ostapenko N. A.
Subject
Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering
Reference12 articles.
1. M.A. Zubin, F.A. Maksimov, and N.A. Ostapenko, “Distinctive Features of the Shock Layer Flow Structure in Conical Gas Flows,” Fluid Dynamics 49(6), 804–818 (2014)
2. M.A. Zubin, F.A. Maksimov, and N.A. Ostapenko, “Criteria of the Existence of Inviscid Vortex Structures in the Shock Layers of Conical Gas Flows,” Dokl. Ross. Akad. Nauk 434, 282 (2014).
3. R. Marsillo, “Vortical Solutions in Supersonic Flows,” AIAA J. 31, 1651 (1993).
4. Yu.P. Gun’ko, A.N. Kudryavtsev, and R.D. Rakhimov, “Supersonic Inviscid Corner Flows with Regular and Irregular Shock Interaction,” Fluid Dynamics 39(2), 304 (2004).
5. A.N. Kraiko, Theoretical Gasdynamics. Classics and State of the Art [in Russian], Torus Press, Moscow (2010).
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