Experimental study of the interaction of shock waves with the contact boundary and zone of turbulent mixing of different gases

التفاصيل البيبلوغرافية
العنوان: Experimental study of the interaction of shock waves with the contact boundary and zone of turbulent mixing of different gases
المؤلفون: O. L. Krivonos, E. A. Sotskov, S. V. Frolov, N. V. Nevmerzhitskii, A. N. Razin, E. V. Bodrov, K. V. Anisiforov, E. V. Levkina, E. D. Sen’kovskii
المصدر: Journal of Applied Mechanics and Technical Physics. 58:200-208
بيانات النشر: Pleiades Publishing Ltd, 2017.
سنة النشر: 2017
مصطلحات موضوعية: Shock wave, Astrophysics::High Energy Astrophysical Phenomena, 02 engineering and technology, Mach wave, 01 natural sciences, Moving shock, 010305 fluids & plasmas, Physics::Fluid Dynamics, symbols.namesake, Optics, 0203 mechanical engineering, Schlieren, 0103 physical sciences, Bow shock (aerodynamics), Shock tube, Physics, business.industry, Mechanical Engineering, Mechanics, Condensed Matter Physics, 020303 mechanical engineering & transports, Mach number, Mechanics of Materials, symbols, Oblique shock, business
الوصف: The interaction of a shock wave with turbulent flow was experimentally investigated. The case where a shock wave formed at one end of the tube, passed through the interface between two quiescent gases with different densities (air–CO2 or air–Ar), was reflected from the end of the tube, and interacted with the zone of turbulent mixing formed at the interface. The Mach number of the shock wave incident on the interface in air was M ≈ 2.37–2.57. The flow field was recorded using the schlieren method and high-speed video recording. It was found that after passing the mixing zone, the shock-wave front was deformed and became unstable.
تدمد: 1573-8620
0021-8944
URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_________::391b8d5d1fb1071ceee609b3d683b3ee
https://doi.org/10.1134/s002189441702002x
حقوق: CLOSED
رقم الأكسشن: edsair.doi...........391b8d5d1fb1071ceee609b3d683b3ee
قاعدة البيانات: OpenAIRE