Dmitry Khotyanovsky

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Coauteurs

Alexey N. KudryavtsevInstitute of Theoretical and Applied MechanicsAdresse e-mail validée de itam.nsc.ru
Mikhail IvanovITAM, Novosibirsk, Russia Adresse e-mail validée de itam.nsc.ru
Yevgeniy A. BondarITAM (Kristianovich Institute of Theoretical and Applied Mechanics), Novosibirsk, RussiaAdresse e-mail validée de itam.nsc.ru
Georgy ShoevITAMAdresse e-mail validée de itam.nsc.ru
Abdellah HadjadjINSA of RouenAdresse e-mail validée de coria.fr
Doyle KnightProfessor of Aerospace and Mechanical Engineering, Rutgers UniversityAdresse e-mail validée de soe.rutgers.edu
Antony Shershneffscientific researcher, Institute of Theoretical and Applied MechanicsAdresse e-mail validée de itam.nsc.ru
Ben-Dorben gurion universityAdresse e-mail validée de bgu.ac.il
Tov Elperinben-gurion university of the negevAdresse e-mail validée de bgu.ac.il
Shigeru YonemuraInstitute of Fluid Science, Tohoku University, Osaka UniversityAdresse e-mail validée de ifs.tohoku.ac.jp
Alexander V. OmelchenkoHigher School of Economics - Saint PetersburgAdresse e-mail validée de hse.ru
Sergey GimelsheinResearch Associate Professor, University of Southern CaliforniaAdresse e-mail validée de usc.edu
Alexander Kosinovhead of laboratory, ITAM SB RAS, Novosibirsk, RussiaAdresse e-mail validée de itam.nsc.ru
Kaoru MarutaProfessor of Institute of Fluid Science, Tohoku UniversityAdresse e-mail validée de ifs.tohoku.ac.jp
Aldo BonfiglioliAssociate Professor of Fluid Machinery, University of Basilicata, ItalyAdresse e-mail validée de unibas.it
Francesco NasutiSapienza University of RomeAdresse e-mail validée de uniroma1.it
Renato PaciorriProfessor of Gasdynamics, University of Rome "La Sapienza"Adresse e-mail validée de uniroma1.it
Andrey Ovsyannikov, PhDIntel CorporationAdresse e-mail validée de intel.com

Dmitry Khotyanovsky

Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences

Adresse e-mail validée de itam.nsc.ru

Computational Fluid Dynamics High-performance computing Supersonic flow Hydrodynamic stability and Transition to turbulence


Titre Trier par citations Trier par année Trier par titre	Citée par Citée par	Année
Transition between regular and Mach reflection of shock waves: new numerical and experimental results MS Ivanov, D Vandromme, VM Fomin, AN Kudryavtsev, A Hadjadj, ... Shock Waves 11 (3), 199-207, 2001	99	2001
Localized Flow Control by Laser Energy Deposition Applied to Edney IV and Intersecting Shocks R Adelgren, H Yan, G Elliott, D Knight, T Beutner, A Zheltovodov, ...	64	2003
The reflection of asymmetric shock waves in steady flows: A numerical investigation MS Ivanov, G Ben-Dor, T Elperin, AN Kudryavtsev, DV Khotyanovsky Journal of Fluid Mechanics 469, 71-87, 2002	63	2002
Flow-Mach-Number-Variation-Induced Hysteresis in Steady Shock Wave Reflections. MS Ivanov, G Ben-Dor, T Elperin, AN Kudryavtsev, DV Khotyanovsky AIAA Journal 39 (5), 972-974, 2001	51	2001
Numerical investigations of transition between regular and Mach reflections caused by free-stream disturbances AN Kudryavtsev, DV Khotyanovsky, MS Ivanov, A Hadjadj, D Vandromme Shock Waves 12 (2), 157-165, 2002	46	2002
Experiments on shock wave reflection transition and hysteresis in low-noise wind tunnel, MS Ivanov, AN Kudryavtsev, SB Nikiforov, DV Khotyanovsky, AA Pavlov Physics of Fluids 15 (6), 1807-1810, 2003	43	2003
Experimental and numerical study of the transition between regular and Mach reflections of shock waves in steady flows MS Ivanov, GP Klemenkov, AN Kudryavtsev, SB Nikiforov, AA Pavlov, ... The 21st International Symposium on Shock Waves, 1997	38	1997
Применение схем высокого порядка точности при моделировании нестационарных сверхзвуковых течений АН Кудрявцев, ТВ Поплавская, ДВ Хотяновский Математическое моделирование 19 (7), 39–55, 2007	34	2007
DSMC and Navier-Stokes Study of Backflow for Nozzle Plumes Expanding into Vacuum PV Vashchenkov, AN Kudryavtsev, DV Khotyanovsky, MS Ivanov. 24th International Symposium on Rarefied Gas Dynamics 762, 355-360, 2005	29	2005
Viscosity effects on weak irregular reflection of shock waves in steady flow MS Ivanov, YA Bondar, DV Khotyanovsky, AN Kudryavtsev, GV Shoev Progress in aerospace sciences 46 (2-3), 89-105, 2010	25	2010
Application of high-order accuracy schemes to numerical simulation of unsteady supersonic flows AN Kudryavtsev, TV Poplavskaya, DV Khotyanovsky Matematicheskoe modelirovanie 19 (7), 39-55, 2007	25	2007
Numerical study of backflow for nozzle plumes expanding into vacuum M Ivanov, A Kudryavtsev, G Markelov, P Vashchenkov, D Khotyanovsky, ... 37th AIAA Thermophysics Conference, 2687, 2004	23	2004
Effects of a Single-pulse Energy Deposition on Steady Shock Wave Reflection DV Khotyanovsky, AN Kudryavtsev, MS Ivanov Shock Waves 15 (5), 353-362, 2006	22	2006
Direct numerical simulation of transition to turbulence in a supersonic boundary layer AN Kudryavtsev, DV Khotyanovsky. Thermophysics and Aeromechanics 22 (5), 559–568, 2015	21	2015
Viscous effects in steady reflection of strong shock waves DK Khotyanovsky, YA Bondar, AN Kudryavtsev, GV Shoev, MS Ivanov AIAA journal 47 (5), 1263-1269, 2009	21	2009
Numerical investigation of high speed free shear flow instability and Mach wave radiation AN Kudryavtsev, DV Khotyanovsky International Journal of Aeroacoustics 4 (3), 325-343, 2005	19	2005
Numerical study of transition between steady regular and Mach reflection caused by free-stream perturbations DV Khotyanovsky, AN Kudryavtsev, MS Ivanov Proc. of 22nd Int. Symp. on Shock Waves (London, UK, 1261-1266, 1999	17	1999
HyCFS, a high-resolution shock capturing code for numerical simulation on hybrid computational clusters AA Shershnev, AN Kudryavtsev, AV Kashkovsky, DV Khotyanovsky AIP Conference Proceedings 1770 (1), 030076, 2016	15	2016
Numerical simulation of the evolution of unstable disturbances of various modes and initial stages of the laminar-turbulent transition in the boundary layer at the freestream … DV Khotyanovsky, AN Kudryavtsev Thermophysics and Aeromechanics 23 (6), 809–818, 2016	11	2016
Переход между регулярным и маховским отражением ударных волн: новые численные и экспериментальные результаты МС Иванов, АН Кудрявцев, СБ Никифоров, ДВ Хотяновский Аэромеханика и газовая динамика, 3-15, 2002	11	2002

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