Author:
Mironov S. G.,Poplavskaya T. V.,Kirilovskiy S. V.
Subject
Nuclear and High Energy Physics,Radiation
Reference6 articles.
1. I.A. Bedarev, S.G. Mironov, K.M. Serdyuk, A.V. Fedorov, and V.M. Fomin, Physical and mathematical modeling of a supersonic flow around a cylinder with a porous insert, J. Appl. Mech. Tech. Phys., 2011. Vol. 52, No. 1, P. 9–17.
2. S.G. Mironov, A.A. Maslov, T.V. Poplavskaya, and S.V. Kirilovskiy, Modeling of a supersonic flow around a cylinder with a gas-permeable porous insert, J. Appl. Mech. Tech. Phys., 2015. Vol. 56, No. 4, P. 549–557.
3. RF Patent 2559193-1, MPK51 V64S21/04, V64S19/00. A method to control the flow around a supersonic aircraft, S.G. Mironov, A.A. Maslov, and I.S. Tsyryulnikov; Applicant and Patent Holder–Novosibirsk State University, No. 2014116998-11; filing date of application 25.04.2014, publication date 10.08.2015, Bull. No. 22.
4. S.G. Mironov, A.A. Maslov, and I.S. Tsyryulnikov, Controlling aerodynamic forces with the help of gas-permeable porous materials, Technical Physics Letters, 2014. Vol. 40, Iss. 10, P. 868–870.
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