Recent Publications



2007

A.N.Kudryavtsev, T.V.Poplavskaya, and D.V.Khotyanovsky. Application of high-order schemes to numerical simulation of unsteady supersonic flow. submitted to Mathematical Modeling (in Russian).
E.G.Ivanov, O.N.Glushchenko, H.Andrae, and A.N.Kudryavtsev. Automatical parallel generation of tetrahedral grids via computational domain decomposition. submitted to Journal of Computational Mathematics and Mathematical Physics (in Russian).
A.N.Kudryavtsev, S.G.Mironov, T.V.Poplavskaya, and I.S.Tsyryulnikov. Airflow effect on evolution of disturbances in hypersonic shock layer on a flat plate. Submitted to 13th International Conference on the Methods of Aerophysical Research (ICMAR-2007), Novosibirsk, Russia, 2007.
A.N.Kudryavtsev, S.G.Mironov, T.V.Poplavskaya, and I.S.Tsyryulnikov. Evolution of disturbances generated by blowing and suction in hypersonic shock layer on a flat plate. Submitted to 13th International Conference on the Methods of Aerophysical Research (ICMAR-2007), Novosibirsk, Russia, 2007.

2006

B.I.Reznikov, Yu.P.Golovachov, A.A.Schmidt, M.S.Ivanov and A.N.Kudryavtsev. Coolant film flow over the edge of a nozzle in a rarefied gas. Technical Physics, Vol.51, No.3, 2006, pp.322-329 (translated from Russian, Zhurnal Tekhnicheskoi Fiziki, Vol.76, No.3, 2006, pp.30-37).
A.N.Kudryavtsev, A.A.Maslov, S.G.Mironov, T.V.Poplavskaya, and I.S.Tsyryulnikov. Direct numerical simulation of hypersonic shock layer receptivity to natural and artificial disturbances. Computational Technologies, Vol.11, Special issue, Pt. 1, 2006, pp.108-116 (in Russian).
A.V.Trotsyuk, A.N.Kudryavtsev, and M.S.Ivanov. Numerical investigation of standing detonation waves. Computational Technologies, Vol.11, Special issue, Pt. 2, 2006, pp.37-44 (in Russian).
D.V.Khotyanovsky, A.N.Kudryavtsev, and M.S.Ivanov. Effects of a single-pulse energy deposition on steady shock wave reflection. Shock Waves, Vol.15, No.5, 2006, pp.353-362.
A.N.Kudryavtsev, S.G.Mironov, T.V.Poplavskaya, and I.S.Tsyryulnikov. Experimental investigation and direct numerical simulation of development of disturbances in the viscous shock layer over a flat plate. Journal of Applied Mechanics and Technical Physics, Vol.47, No.5, 2006, pp.3-15 (in Russian).
Yu.P.Gounko and A.N.Kudryavtsev. Numerical simulation of free shock interaction in corner flows. Thermophysics and Aeromechanics, Vol.13, No.2, 2006, pp.239-256 (in Russian).
E.G.Ivanov, H.Andrae, and A.N.Kudryavtsev. Domain decomposition approach for automatic parallel generation of tetrahedral grids. Computational Methods in Applied Mathematics, Vol.6, No.2, 2006, pp.178-193.
E.G.Ivanov, H.Andrae, and A.N.Kudryavtsev. Domain decomposition approach for automatic parallel generation of tetrahedral grids. Berichte des Fraunhofer Institut Techno- und Wirtschaftsmathematik (ITWM), Nr. 87, 2006.
A.N.Kudryavtsev and D.V.Khotyanovsky. Application of WENO schemes for numerical simulations of high-speed flows. Accepted for presentation on 4th International Conference on Computational Fluid Dynamics (Ghent, Belgium, July 10-14, 2006).
A.N.Kudryavtsev, S.G.Mironov, T.V.Poplavskaya, and I.S.Tsyryulnikov. Numerical simulation of flat plate hypersonic shock layer perturbed by external acoustic waves. Accepted for presentation on 4th International Conference on Computational Fluid Dynamics (Ghent, Belgium, July 10-14, 2006).
A.N.Kudryavtsev, S.G.Mironov, T.V.Poplavskaya, and I.S.Tsyryulnikov. Numerical and experimental investigation of mean flow and instability in hypersonic viscous shock layer. Accepted for presentation on 25th International Symposium on Rarefied Gas Dynamics (St. Petersburg, Russia, July 21-28, 2006).
E.G.Ivanov, H.Andrae and A.N.Kudryavtsev. Domain decomposition approach for automatic parallel generation of three-dimensional unstructured grids. Accepted for presentation on ECCOMAS CFD 2006, European Conference on Computational Fluid Dynamics (Egmond aan Zee, The Netherlands, September 5-8, 2006).
A.N.Kudryavtsev and D.V.Khotyanovsky. Numerical simulation of shock-dominated flows with WENO schemes. Accepted for presentation on 5th Asia Workshop on Computational Fluid Dynamics (Xi'an, China, August 20-23, 2006).
A.N.Kudryavtsev and D.V.Khotyanovsky. Numerical simulation of 3D shock wave configurations in pulse jets issuing from orifices of different shapes. Accepted for presentation on 17th International Shock Interaction Symposium (Rome, Italy, September 4-8, 2006).
M.S.Ivanov, A.N.Kudryavtsev and D.V.Khotyanovsky. Weak Mach reflection in steady flow. Accepted for presentation on 17th International Shock Interaction Symposium (Rome, Italy, September 4-8, 2006).
E.G.Ivanov, H.Andrae, and A.N.Kudryavtsev. Automatic parallel generation of tetrahedral grids by using a domain decomposition approach. Accepted for presentation on International Conference on Numerical Grid Generation (Moscow, Russia, July 5-8, 2006).

2005

A.Hadjadj and A.N.Kudryavtsev. Computation and flow visualization in high-speed aerodynamics. Journal of Turbulence, Vol.6, 2005, pp.1-25.
A.N.Kudryavtsev and D.V.Khotyanovsky. Numerical investigation of high speed free shear flow instability and Mach wave radiation. International Journal of Aeroacoustics, Vol.4, No.3&4, 2005, pp.267-286.
A.V.Trotsyuk, A.N.Kudryavtsev and M.S.Ivanov. Numerical study of standing gas detonation waves. Proceedings of European Conference for Aerospace Sciences (EUCASS), Moscow, Russia, July 4-7, 2005. 9 p.

2004

A.Hadjadj, A.N.Kudryavtsev, and M.S.Ivanov. Numerical investigation of shock-reflection phenomena in overexpanded supersonic jets. AIAA Journal, Vol.42, No.3, 2004, pp.570-577.
Yu.P.Goonko, A.N.Kudryavtsev, and R.D.Rakhimov. Supersonic inviscid corner flows with regular and irregular shock interactions. Mekhanika Zhidkosti i Gaza, 2004, No. 2, pp.152-169 (in Russian).
A.V.Trotsyuk, A.N.Kudryavtsev, and M.S.Ivanov. Computational study of Mach reflection in chemically reacting steady flows. AIAA Paper No.2004-0271, 2004, 11 p.
M.S.Ivanov, D.V.Khotyanovsky, A.N.Kudryavtsev, P.V.Vashchenkov, G.N.Markelov, and A.A.Schmidt. Numerical study of backflow for nozzle plumes expanding into vacuum. AIAA Paper No.2004-2687, 2004, 16 p. (PDF, 4.4 Mb)
A.V.Trotsyuk, A.N.Kudryavtsev, and M.S.Ivanov. Numerical investigations of detonation waves in supersonic steady flows. Application of Detonation to Propulsion. Ed. by G.Roy, S.Frolov, J.Shepherd. Torus Press: Moscow, 2004, pp.167-173.
Yu.P.Goonko, A.N.Kudryavtsev, and A.Chpoun. 3D interaction of shock waves in corner flow. Proceedings of the 24th International Symposium on Shock Waves (Beijing, China, July 11-16, 2004). Ed. by Z.L.Jiang, Springer, Vol.1, pp.437-442. (PDF, 752 kb)
A.V.Trotsyuk, A.N.Kudryavtsev, and M.S.Ivanov. Numerical simulation of steady shock and detonation wave configurations in a supersonic chemically reacting flow. Proceedings of the 24th International Symposium on Shock Waves (Beijing, China, July 11-16, 2004). Ed. by Z.L.Jiang, Springer, Vol.1, pp.511-516. (PDF, 338 kb)
M.S.Ivanov, A.N.Kudryavtsev, S.B.Nikiforov, A.D.Kosinov, and A.A.Pavlov. Experimental investigation of strong shock reflection and and hysteresis in various wind tunnels. Proceedings of the 24th International Symposium on Shock Waves (Beijing, China, July 11-16, 2004). Ed. by Z.L.Jiang, Tsinghua Univ. Press, Paper No. 1381, 6 p. (PDF, 752 kb)
M.S.Ivanov, A.M.Kharitonov, D.V.Khotyanovsky, A.N.Kudryavtsev, S.B.Nikiforov, and A.A.Pavlov. Three-dimensional steady shock wave interactions. Numerical simulations and experimental validation. European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2004), Jyvaskyla, Finland, July 24-28, 2004. Proceedings, Vol. II, ISBN 951-39-1869-6. Paper No. 543, 16 p. (PDF, 717 kb)
D.V.Khotyanovsky, A.N.Kudryavtsev, D.D.Knight, and M.S.Ivanov. Control of shock wave interaction by impulse laser energy deposition. European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2004), Jyvaskyla, Finland, July 24-28, 2004. Proceedings, Vol. II, ISBN 951-39-1869-6. Paper No. 546, 11 p. (PDF, 639 kb)
Yu.P.Golovachov, M.S.Ivanov, D.V.Khotyanovsky, A.N.Kudryavtsev, B.I.Reznikov, A.A.Smirnovsky, and A.A.Schmidt. Multiphase three-component nozzle flow (model validation). European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2004), Jyvaskyla, Finland, July 24-28, 2004. Proceedings, Vol. II, ISBN 951-39-1869-6. Paper No. 750, 20 p. (PDF, 367 kb)
M.S.Ivanov, D.V.Khotyanovsky, A.N.Kudryavtsev, S.B.Nikiforov, and A.V.Trotsyuk. Hysteresis-related phenomena in shock wave reflection. XXI International Congress of Theoretical and Applied Mechanics (Warsaw, Poland, August 15-21, 2004). Proceedings, ISBN 83-89697-01-1, Paper No. FM5-10531, 2 p. (PDF, 94 kb)
A.N.Kudryavtsev and D.V.Khotyanovsky. Development and practical application of WENO schemes for compressible fluid flow computations. XXI International Congress of Theoretical and Applied Mechanics (Warsaw, Poland, August 15-21, 2004). Proceedings, ISBN 83-89697-01-1, Paper No. FM6-11485, 2 p. (PDF, 302 kb)
Yu.P.Goonko and A.N.Kudryavtsev. On some properties of supersonic corner flows formation. Proceedings of the 12th International Conference on the Methods of Aerophysical Research (ICMAR-2004), Novosibirsk, Russia, 28 June - 3 July 2004, Part I, pp. 100-105.
A.V.Trotsyuk, A.N.Kudryavtsev and M.S.Ivanov. Numerical simulation of detonation waves in supersonic steady flows. Proceedings of International Conference on Combustion and Detonation - Zel'dovich Memorial (Moscow, Russia, August 30 - September 3, 2004). Ed. by A.Borisov, S.Frolov, and A.Kuhl. Paper No. PP4-15, 26 p.
Yu.P.Golovachov, B.I.Reznikov, A.A.Smirnovsky, A.A.Schmidt, M.S.Ivanov, and A.N.Kudryavtsev. Desintegration of cooling film at the nozzle lip as an origin of spaceraft external atmosphere. To be published in Proceedings of International Conference on Fundamental Problems of High-Speed Flows (Zhukovsky, Russia, September 21-24), 5 p. (in Russian) (DOC, 118 kb)

2003

M.S.Ivanov, A.N.Kudryavtsev, S.B.Nikiforov, D.V.Khotyanovsky, and A.A.Pavlov. Experiments on shock wave reflection transition and hysteresis in low-noise wind tunnel. Physics of Fluids, Vol.15, No.6, 2003, pp.1807-1810.
A.-S.Mouronval, A.Hadjadj, A.N.Kudryavtsev, and D.Vandromme. Numerical investigation of transient nozzle flow. Shock Waves, Vol.12, No.5, 2003, pp.403-411. (PDF, 1.1 Mb)
A.V.Trotsyuk, A.N.Kudryavtsev, and M.S.Ivanov. Numerical investigation of unsteady Mach reflection of detonation waves. Computational Fluid Dynamics Journal, Vol.12, No.2, 2003, pp.248-257. (gzipped PS, 326 kb)
M.S.Ivanov, A.N.Kudryavtsev, S.B.Nikiforov, A.A.Pavlov, and A.N.Shiplyuk. Study of transition between regular and Mach reflections in different wind tunnels. AIAA Paper No.2003-0156, 2003, 10 p.
Yu.P.Golovachov, M.S.Ivanov, D.V.Khotyanovsky, A.N.Kudryavtsev, V.A.Mazurkevich, B.I.Reznikov, A.A.Schmidt. Numerical simulation of a multiphase three-component flow in a supersonic nozzle. AIAA Paper No.2003-3439, 2003, 12 p.
D.V.Khotyanovsky, D.D.Knight, A.N.Kudryavtsev, and M.S.Ivanov. Numerical study on laser-induced shock wave reflection transition. Shock Wave/Vortex Ineraction. Proceedings of 5th International Workshop on Shock/Vortex Interaction (Kaohsiung, Taiwan, October 27-31, 2003). Ed. by S.M.Liang, pp.84-90. (DOC, 575 kb)
D.V.Khotyanovsky, D.D.Knight, A.N.Kudryavtsev, and M.S.Ivanov. Parallel simulation of laser-induced shock wave reflection transition. Parallel Computational Fluid Dynamics. Proceedings of Parallel CFD 2003 Conference (Moscow, Russia, May 13-15, 2003). Ed. by B.Chetverushkin, A.Ecer, J.Periaux, N.Satofuka, and P.Fox, pp.365-372. (PDF, 542 kb)
A.V.Trotsyuk, A.N.Kudryavtsev, and M.S.Ivanov. Mach reflection of shock and detonation waves in steady supersonic chemically reacting flows. Proceedings of International Conference on Recent Advances in Space Technologies (Istanbul, Turkey, November 20-22, 2003), Ed. by S.Kurnaz, F.Ince, and S.Onbasioglu, pp.491-499.
A.V.Trotsyuk, A.N.Kudryavtsev, and M.S.Ivanov. Numerical simulation of reflection of detonation and shock waves in supersonic flows. Confined Detonation and Pulse Detonation Engines. Ed. by G.Roy, S.Frolov, R.Santoro, S.Tsyganov. Torus Press: Moscow, 2003, pp.73-86.

2002

M.S.Ivanov, G.Ben-Dor, T.Elperin, A.N.Kudryavtsev, and D.V.Khotyanovsky. The reflection of asymmetric shock waves in steady flows: a numerical investigation. Journal of Fluid Mechanics, Vol.469, 2002, pp.71-87. (PDF, 669 kb)
A.N.Kudryavtsev, D.V.Khotyanovsky, M.S.Ivanov, A.Hadjadj, and D.Vandromme. Numerical investigation of transition between regular and Mach reflections caused by free-stream disturbances. Shock Waves, Vol.12, No.2, 2002, pp.157-165. (PDF, 317 kb)
M.S.Ivanov, A.N.Kudryavtsev, S.B.Nikiforov, and D.V.Khotyanovsky. Transition between regular and Mach reflection of shock waves: new numerical and experimental results. Aeromechanics and Gas Dynamics, 2002, No.3, pp.3-12 (in Russian). (PDF, 373 kb)
S.F.Gimelshein, D.A.Levin, G.N.Markelov, A.N.Kudryavtsev, M.S.Ivanov. Statistical simulation of laminar separation in hypersonic flows: numerical challenges. AIAA Paper No.2002-0736, 2002, 13 p.
A.N.Kudryavtsev, D.V.Khotyanovsky, M.S.Ivanov, A.Hadjadj, and D.Vandromme. Transition between regular and Mach shock reflections in plane overexpanded jets. AIAA Paper No.2002-0977, 2002, 11 p. (gzipped PS, 1.5 Mb)
D.Khotyanovsky and A.Kudryavtsev. Large eddy simulation of non-isobaric supersonic jets. Advances in Turbulence IX, Proceedings of the Ninth European Turbulence Conference, I.P.Castro et al. (Eds.), Southampton, UK, July 2-5, 2002, pp.813-816. (gzipped PS, 695 kb)
Yu.P.Goonko, A.N.Kudryavtsev and R.D.Rakhimov. Supersonic inviscid flows with three-dimensional interaction of shock waves in corners formed by intersecting wedges. Proceedings of the 11th International Conference on the Methods of Aerophysical Research (ICMAR-2002), Novosibirsk, Russia, 1-7 July 2002, Part I, pp. 79-85.
A.V.Trotsyuk, A.N.Kudryavtsev and M.S.Ivanov. Numerical investigation of interaction of oblique shock and detonation waves in a steady supersonic flow of a chemically reactive gaseous mixture. Proceedings of the 11th International Conference on the Methods of Aerophysical Research (ICMAR-2002), Novosibirsk, Russia, 1-7 July 2002, Part I, pp. 183-188.
A.Hadjadj and A.N.Kudryavtsev. Turbulence modeling validation for afterbody flows. Proceedings of the 11th International Conference on the Methods of Aerophysical Research (ICMAR-2002), Novosibirsk, Russia, 1-7 July 2002, Part II, pp. 73-78.
V.I.Zapryagaev, A.N.Kudryavtsev, A.V.Lokotko, A.V.Solotchin, A.A.Pavlov, and A.Hadjadj. An experimental and numerical study of a supersonic-jet shock-wave structure. Proceedings of the 11th International Conference on the Methods of Aerophysical Research (ICMAR-2002), Novosibirsk, Russia, 1-7 July 2002, Part II, pp. 187-191.
A.N.Kudryavtsev, D.V.Khotyanovsky, A.Hadjadj, D.Vandromme, and M.S.Ivanov. Numerical investigation of shock wave interactions in supersonic imperfectly expanded jets. Proceedings of the 11th International Conference on the Methods of Aerophysical Research (ICMAR-2002), Novosibirsk, Russia, 1-7 July 2002, Part III, pp. 138-143.
M.S.Ivanov, D.V.Khotyanovsky, A.N.Kudryavtsev, S.B.Nikiforov, and A.A.Pavlov. Study of transition between steady regular and Mach reflections in a quiet wind tunnel. West East High Speed Flow Fields. Aerospace applications from high subsonic to hypersonic regime. Proceedings of WEHSFF 2002 Conference (Marseille, France, April 22-26, 2002). Ed. by D.E.Zeitoun, J.Periaux, J.A.Desideri, and M.Marini. CIMNE, Barcelona, 2003, pp.265-273.
D.V.Khotyanovsky, A.N.Kudryavtsev, M.S.Ivanov, B.Chanetz, A.Durand, M.V.Chernyshev, A.V.Omelchenko, and V.N.Uskov. Analytical, numerical and experimental investigation of shock wave reflection transition induced by variation of distance between wedges. West East High Speed Flow Fields. Aerospace applications from high subsonic to hypersonic regime. Proceedings of WEHSFF 2002 Conference (Marseille, France, April 22-26, 2002). Ed. by D.E.Zeitoun, J.Periaux, J.A.Desideri, and M.Marini. CIMNE, Barcelona, 2003, pp.274-281.
A.N.Kudryavtsev, A.Hadjadj, D.V.Khotyanovsky, M.S.Ivanov, and D.Vandromme. Numerical study of shock reflection phenomena in overexpanded jets. West East High Speed Flow Fields. Aerospace applications from high subsonic to hypersonic regime. Proceedings of WEHSFF 2002 Conference (Marseille, France, April 22-26, 2002). Ed. by D.E.Zeitoun, J.Periaux, J.A.Desideri, and M.Marini. CIMNE, Barcelona, 2003, pp.322-329.
V.I.Zapryagaev, A.N.Kudryavtsev, A.V.Lokotko, A.V.Solotchin, A.A.Pavlov, and A.Hadjadj. Experimental and numerical investigation of shock-wave structure of supersonic jet. West East High Speed Flow Fields. Aerospace applications from high subsonic to hypersonic regime. Proceedings of WEHSFF 2002 Conference (Marseille, France, April 22-26, 2002). Ed. by D.E.Zeitoun, J.Periaux, J.A.Desideri, and M.Marini. CIMNE, Barcelona, 2003, pp.346-351.

2001

M.S.Ivanov, G.Ben-Dor, T.Elperin, A.N.Kudryavtsev, and D.V.Khotyanovsky. Mach-number-variation-induced hysteresis in steady flow shock wave reflections. AIAA Journal, Vol.39, No.5, 2001, pp.972-974.
M.S.Ivanov, D.Vandromme, V.M.Fomin, A.N.Kudryavtsev, A.Hadjadj, and D.V.Khotyanovsky. Transition between regular and Mach reflection of shock waves: new numerical and experimental results. Shock Waves, Vol.11, No.3, 2001, pp.197-207. (PDF, 353 kb)
Yu.P.Gun'ko, A.N.Kudryavtsev, I.I.Mazhul', R.D.Rakhimov, and A.M.Kharitonov. Gasdynamics of a convergent air-intake with a nose compression surface. Fluid Dynamics, Vol.36, No.2, 2001, pp.312-322 (translated from Russian, Mekhanika Zhidkosti i Gaza, 2001, No.2, pp.157-169).
Yu.P.Goonko, A.N.Kudryavtsev, I.I.Mazhul, and R.D.Rakhimov. Comparative study of flows over 2D flat and 3D convergent inlets integrated with hypersonic airplanes. Thermophysics and Aeromechanics, Vol.8, No.1, 2001, pp.25-37 (translated from Russian, Teplofizika i Aeromekhanika, Vol.8, No.1, 2001, pp.27-40).
A.V.Trotsyuk, A.N.Kudryavtsev, and M.S.Ivanov. Non-self-similarity in unsteady Mach reflection of detonation waves. AIAA Paper No.2001-3940, 2001, 9 p.
D.V.Khotyanovsky, A.N.Kudryavtsev, and M.S.Ivanov. Numerical study of peculiarities of asymmetrical reflection of steady shock waves. AIAA Paper No.2001-2893, 2001, 10 p.
M.S.Ivanov, A.M.Kharitonov, D.V.Khotyanovsky, A.N.Kudryavtsev, G.N.Markelov, and S.B.Nikiforov. Numerical and experimental study of 3D steady shock wave interactions. AIAA Paper No.2001-0740, 2001, 10 p.
D.V.Khotyanovsky, A.N.Kudryavtsev, and M.S.Ivanov. On possibility of strong regular reflection of asymmetric steady shock waves. Proceedings of Symposium on Shock Waves (Japan, March 8-10, 2001), pp.295-298.
M.S.Ivanov, D.V.Khotyanovsky, A.N.Kudryavtsev, G.N.Markelov, and S.B.Nikiforov. Experimental study of 3D shock wave configurations during RR <--> MR transition. Proceedings of Symposium on Shock Waves (Japan, March 8-10, 2001), pp.443-446.
A.N.Kudryavtsev and A.Hadjadj. Visualisation graphique en mecanique des fluides numerique. Proceedings of 9eme Colloque Francophone de Visualisation et traitement d'images en mecanique des fluides, FLUVISU 2001 (Rouen, France, June 18-21, 2001), pp.55-62 (in French). (gzipped PS, 1.1 Mb)
G.N.Markelov, A.N.Kudryavtsev, and M.S.Ivanov Rarefaction effects on separation of hypesonic laminar flows. Proceedings of 22nd International Symposium on Rarefied Gas Dynamics (Sydney, Australia, July 9-14, 2000), American Institute of Physics Conference Proceedings, Vol.585, Melville, N.Y., 2001, pp.707-714.
M.S.Ivanov, D.V.Khotyanovsky, A.N.Kudryavtsev, and S.B.Nikiforov. Experimental study of 3D shock wave configurations during RR <-> MR transition. Proceedings of 23rd International Symposium on Shock Waves (Fort Worth, USA, July 22-27, 2001), pp.1462-1470. (gzipped PS, 885 kb)
D.V.Khotyanovsky, A.N.Kudryavtsev, G.Ben-Dor, and M.S.Ivanov. Strong regular reflection of steady shock waves. Proceedings of 23rd International Symposium on Shock Waves (Fort Worth, USA, July 22-27, 2001), pp.1471-1478. (gzipped PS, 558 kb)
A.N.Kudryavtsev, A.Hadjadj, D.Vandromme, and M.S.Ivanov. Numerical simulation of shock wave reflection in overexpanded exhaust jets. Proceedings of 23rd International Symposium on Shock Waves (Fort Worth, US, July 22-27, 2001), pp.712-718. (gzipped PS, 353 kb)
Yu.P.Goonko, A.N.Kudryavtsev, I.I.Mazhul, and R.D.Rakhimov. Investigations of lifting bodies waveriders, and inlets with convergent compression surfaces. Proceedings of 4th European Symposium on Aerothermodynamics for Space Vehicles (Capua, Italy, October 15-18, 2001), pp.175-182.
M.S.Ivanov, A.N.Kudryavtsev, D.V.Khotyanovsky, and S.B.Nikiforov. New experimental and numerical results on transition between steady regular and Mach reflections. Proceedings of 4th European Symposium on Aerothermodynamics for Space Vehicles (Capua, Italy, October 15-18, 2001), pp.341-347.
A.-S.Mouronval, A.Hadjadj, A.N.Kudryavtsev, and D.Vandromme. Numerical investigation of transient nozzle flow. Proceedings of 4th European Symposium on Aerothermodynamics for Space Vehicles (Capua, Italy, October 15-18, 2001), pp.399-406.

2000

G.N.Markelov, A.N.Kudryavtsev, and M.S.Ivanov. Continuum and kinetic simulation of laminar separated flow at hypersonic speeds. Journal of Spacecraft and Rockets, Vol.37, No.4, 2000, pp.499-506. (gzipped PS, 609 kb)
M.S.Ivanov, A.N.Kudryavtsev, and D.V.Khotyanovsky. Numerical simulation of the transition between the regular and Mach reflection of shock waves under the action of local perturbations. Physics-Doklady, Vol.45, No.7, 2000, pp.353-357 (translated from Russian, Doklady Akademii Nauk, Vol.373, No.3, 2000, pp.332-336). (PDF, 819 kb)
A.Kudryavtsev and D. Khotyanovsky. Numerical simulation of the spatial evolution of the instabilities in a supersonic plane jet. Advances in Turbulence VIII, Proceedings of the Eighth European Turbulence Conference, C. Dopazo et al. (Eds.), Barcelona, Spain, June 27-30, 2000, pp.161-164.
G.Markelov, A.Kudryavtsev, and M.Ivanov. Continuum and kinetic simulation of laminar separation. European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2000). Barcelona, 11-14 September 2000. CD-Rom Proceedings. Paper No. 690, 20 p.
A.N.Kudryavtsev, D.V.Khotyanovsky, and M.S.Ivanov. Numerical simulation of asymmetrical steady shock wave interactions. European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2000). Barcelona, 11-14 September 2000. CD-Rom Proceedings. Paper No. 741, 13 p.
A.Hadjadj, M.S.Ivanov, D.Khotyanovsky, A.N.Kudryavtsev, and D.Vandromme. Further numerical investigations on transition to Mach reflection. European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2000). Barcelona, 11-14 September 2000. CD-Rom Proceedings. Paper No. 742, 18 p.
Yu.P.Goon'ko, A.M.Kharitonov, A.N.Kudryavtsev, I.I.Mazhul, and R.D.Rakhimov. Euler simulations of the flow over a hypersonic convergent inlet integrated with a forebody compression surface. European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2000). Barcelona, 11-14 September 2000. CD-Rom Proceedings. Paper No. 890, 16 p.
Yu.P.Goo'nko, A.N.Kudryavtsev, I.I.Mazhul', and R.D.Rakhimov, A.M.Kharitonov. Gasdynamics of a convergent inlet integrated with a nose convergent compression surface. Proceedings of the 10th International Conference on the Methods of Aerophysical Research (ICMAR-2000), Novosibirsk, Russia, 9-14 July 2000, Vol. 1, pp. 104-109.
Yu.P.Goo'nko, A.N.Kudryavtsev, I.I.Mazhul', and R.D.Rakhimov. Some features of flows around hypersonic aircraft forebodies integrated with 2D flat and 3D convergent inlets. Proceedings of the 10th International Conference on the Methods of Aerophysical Research (ICMAR-2000), Novosibirsk, Russia, 9-14 July 2000, Vol. 1, pp. 110-115.
M.S.Ivanov, A.N.Kudryavtsev, D.V.Khotyanovsky, and G.N.Markelov. Numerical study of 3D regular and Mach reflections of steady shock waves. Proceedings of the 10th International Conference on the Methods of Aerophysical Research (ICMAR-2000), Novosibirsk, Russia, 9-14 July 2000, Vol. 1, pp. 122-127.
M.S.Ivanov, G.P.Klemenkov, A.N.Kudryavtsev, S.B.Nikiforov, A.A.Pavlov, A.M.Kharitonov, and V.M.Fomin. Experimental investigation of 3D steady shock wave interaction. Proceedings of the 10th International Conference on the Methods of Aerophysical Research (ICMAR-2000), Novosibirsk, Russia, 9-14 July 2000, Vol. 1, pp. 128-135.

1999

G.N.Markelov, A.N.Kudryavtsev, and M.S.Ivanov. Continuum and kinetic simulation of shock wave/boundary layer interaction in hypersonic flows. AIAA Paper No.99-3527, 1999, 12 p.
A.N.Kudryavtsev, D.V. Khotyanovsky, G.N.Markelov, and M.S.Ivanov. Numerical simulation of reflection of shock waves generated by finite-width wedge. Proceedings of 22nd International Symposium on Shock Waves, Imperial College, London, UK, July 18-23, 1999, Eds.: G.J.Ball, R.Hillier, G.T.Roberts, pp.1185-1190.
M.S.Ivanov, G.P.Klemenkov, A.N.Kudryavtsev, S.B.Nikoforov, A.A.Pavlov, A.M.Kharitonov, and V.M.Fomin. Wind tunnel experiments on shock wave reflection transition and hysteresis. Proceedings of 22nd International Symposuim on Shock Waves, Imperial College, London, UK, July 18-23, 1999, Eds.: G.J.Ball, R.Hillier, G.T.Roberts, pp.1191-1196.
D.V. Khotyanovsky, A.N.Kudryavtsev, and M.S.Ivanov. Numerical study of transition between steady regular and Mach reflection caused by free-stream perturbations. Proceedings of 22nd International Symposium on Shock Waves, Imperial College, London, UK, July 18-23, 1999, Eds.: G.J.Ball, R.Hillier, G.T.Roberts, pp.1261-1266.
A.M.Kharitonov, V.M.Fomin, M.S.Ivanov, G.P.Klemenkov, A.N.Kudryavtsev, and A.A.Pavlov. Experimental study of the transition between regular and Mach reflection of shock waves in steady flows. Paper of 91st Semiannual Meeting of the Supersonic Tunnel Association International (Bedford, UK), 1999, 11 p.
G.N.Markelov, A.N.Kudryavtsev, and M.S.Ivanov. Numerical modeling of near-continuum flow about a hollow cylinder flare. Proceedings of the 21st International Symposium on Rarefied Gas Dynamics (Marseille, France, 26-31 July 1998). Cepadues Editions. Vol.1, 1999, pp.647-654.

1998

M.S.Ivanov,G.N.Markelov, A.N.Kudryavtsev, and S.F.Gimelshein. Numerical analysis of shock wave reflection transition in steady flows. AIAA Journal, Vol. 36, No. 11, 1998, pp. 2079-2086.
M.S.Ivanov, A.N.Kudryavtsev, S.F.Gimelshein, G.N.Markelov, and D.V.Khotyanovsky. Numerical simulation of three-dimensional regular and Mach reflections of shock waves in steady flows. Computational Fluid Dynamics'98. Proceedings of 4th ECCOMAS CFD Conference (Athens, Greece, 7-11 September 1998). J.Wiley & Sons, Chichester, Vol.1, Part 2, 1998, pp.869-874.
A.N.Kudryavtsev and D.V.Khotyanovsky. Numerical simulation of compressible shear layer development with weighted ENO schemes. Computational Fluid Dynamics'98. Proceedings of 4th ECCOMAS CFD Conference (Athens, Greece, 7-11 September 1998). J.Wiley & Sons, Chichester, Vol.1, Part 2, 1998, pp.900-905.
A.N.Kudryavtsev and R.D.Rakhimov. A marching procedure of numerical solution of two-dimensional and three-dimensional steady Euler equations using shock-capturing schemes. Proceedings of 9th International Conference on Methods of Aerophysical Research (Novosibirsk, Russia, 29 June - 3 July 1998). Part I, 1998, pp.117-122.
Yu.P.Goon'ko, A.N.Kudryavtsev, and R.D. Rakhimov. A numerical study of the methods of reducing the internal nonuniform flows with shock waves to equivalent one-dimensional flows. Proceedings of 9th International Conference on Methods of Aerophysical Research (Novosibirsk, Russia, 29 June - 3 July 1998). Part III, 1998, pp.136-141.
A.N. Kudryavtsev and D.V. Khotyanovsky. A numerical method for simulation of unsteady phenomena in high-speed free shear flows. Proceedings of 9th International Conference on Methods of Aerophysical Research (Novosibirsk, Russia, 29 June - 3 July 1998). Part III, 1998, pp.165-170.
A.N.Kudryavtsev and D.V.Khotyanovsky. Nonlinear evolution of shear layer disturbances in a supersonic plane jet. Proceedings of 9th International Conference on Methods of Aerophysical Research (Novosibirsk, Russia, 29 June - 3 July 1998). Part III, 1998, pp.171-176.
A.N. Kudryavtsev and D. V. Khotyanovsky. Numerical simulation of nonlinear interactions in subsonic and supersonic free shear layers. Proceedings of IUTAM Symposium on Dynamics of Slender Vortices (Aachen, Germany, 31 August - 3 September 1997). Kluwer Academic Publishers, Dordrecht et al., 1998, pp.133-142.
M.S.Ivanov, S.F.Gimelshein, A.N.Kudryavtsev, and G.N. Markelov. Transition from regular to Mach reflection in two- and three-dimensional flows. Proceedings of 21st International Symposium on Shock Waves (Great Keppel, Australia, 20-25 July 1997). Panther Publishing, Fyshwick, Vol.2, 1998, pp.813-818.
M.S. Ivanov, G.P. Klemenkov, A.N. Kudryavtsev, S.B. Nikiforov, A.A.Pavlov, V.M.Fomin, A.M.Kharitonov, D.V.Khotyanovsky, and Hornung H.G. Experimental and numerical study of the transition between regular and Mach reflections of shock waves in steady flows. Proceedings of 21st International Symposium on Shock Waves (Great Keppel, Australia, 20-25 July 1997). Panther Publishing, Fyshwick, Vol.2, 1998, pp.819-824.
A. Hadjadj, A.N. Kudryavtsev, M.S. Ivanov, and D. Vandromme. Numerical investigation of hysteresis effects and slip surface instability in the steady Mach reflection. Proceedings of 21st International Symposium on Shock Waves (Great Keppel, Australia, 20-25 July 1997). Panther Publishing, Fyshwick, Vol.2, 1998, pp.841-847.

1997

M.S. Ivanov, G.P. Klemenkov, A.N. Kudryavtsev, V.M. Fomin, and A.M. Kharitonov. Experimental investigation of the transition to the Mach reflection of steady shock waves. Physics-Doklady, Vol.42, No.12, 1997, pp.691-695 (translated from Russian, Doklady Akademii Nauk, Vol.357, No.5, 1997, pp. 623-627).
M.S. Ivanov,G.N. Markelov, A.N.Kudryavtsev, and S.F.Gimelshein. Transition between regular and Mach reflections of shock waves in steady flows. AIAA Paper No.97-2511, 1997, 13 p.
M.S. Ivanov, S.F. Gimelshein. A.N. Kudryavtsev, and G.N. Markelov. Numerical study of transition criteria from regular to Mach reflection in steady flows by kinetic and continuum approaches. Proceedings of Symposium on Shock Waves, (Tokyo, Japan, 13-15 March 1997), 1997, pp.257-260.
M.S.Ivanov, S.F.Gimelshein, A.N.Kudryavtsev, and G.N.Markelov. Numerical study of the transition from regular to Mach reflection in steady supersonic flows. Proceedings of 15th International Conference on Numerical Methods in Fluid Dynamics (Monterey, CA, USA, 24-28 June 1996). Springer, Lecture Notes in Physics, Vol.490, 1997, pp.394-399.

1996

V.M.Fomin, M.S.Ivanov, A.M.Kharitonov,S.F.Gimelshein, G.P.Klemenkov, A.N.Kudryavtsev, G.N.Markelov, A.A.Pavlov, and H.G.Hornung. Analysis of hysteresis phenomenon in steady interaction of strong shock waves. Proceedings of 8th International Conference on Methods of Aerophysical Research (Novosibirsk, Russia, 2-6 September, 1996), Part 3, 1996, pp.53-61.
A.N.Kudryavtsev and D.V.Khotyanovsky. Implementation of ENO schemes to numerical simulation of supersonic mixing layer instabilities. Proceedings of 8th International Conference on Methods of Aerophysical Research (Novosibirsk, Russia, 2-6 September,1996), Part 3, 1996, pp.178-183.
G.N. Markelov, M.S. Ivanov, A.N.Kudryavtsev, and S.F.Gimelshein. Numerical investigation of the transition from regular to Mach reflection in steady supersonic flows. Proceedings of 8th International Conference on Methods of Aerophysical Research (Novosibirsk, Russia, 2-6 September, 1996), Part 3, 1996, pp.206-211.
A.N.Kudryavtsev. Numerical simulation of nonlinear development of subsonic and supersonic instabilities in compressible shear layers. Computational Fluid Dynamics '96. Proceedings of 3rd European CFD Conference (Paris, France, 9-13 September, 1996). Ed. by J.-A. Desideri, C.Hirsh, P. Le Tallec et al. J.Wiley & Sons, Chichester, 1996, pp.346-351.
M.S.Ivanov, G.N.Markelov, A.N.Kudryavtsev, and S.F.Gimelshein. Numerical investigation of shock wave/boundary layer interaction in the near-continuum hypersonic flow over concave bodies. Computational Fluid Dynamics '96. Proceedings of 3rd European CFD Conference (Paris, France, 9-13 September, 1996). Ed. by J.-A. Desideri, C.Hirsh, P. Le Tallec et al. J.Wiley & Sons, Chichester, 1996, pp.656-661.
V.M.Fomin, H.G.Hornung, M.S.Ivanov, A.M.Kharitonov, G.P.Klemenkov, A.N.Kudryavtsev, and A.A.Pavlov. The study of transition between regular and Mach reflection of shock waves in different wind tunnels. Proceedings of 12th International Mach Reflection Symposium (Pilanesberg, South Africa, 30 June - 4 July, 1996), 1996, pp. 137-151.
M.S.Ivanov,S.F.Gimelshein,A.N.Kudryavtsev, and G.N.Markelov. Numerical analysis of hysteresis phenomenon in steady interactions of strong shock waves. Proceedings of 12th International Mach Reflection Symposium (Pilanesberg, South Africa, 30 June - 4 July, 1996), 1996, pp. 122-136.




Last updated: September 13, 2006.