Welcome to Open Science
Contact Us
Home Books Journals Submission Open Science Join Us News
Development of Cognitive Technology in Computational Aerodynamics
Current Issue
Volume 1, 2014
Issue 1 (April)
Pages: 11-15   |   Vol. 1, No. 1, April 2014   |   Follow on         
Paper in PDF Downloads: 32   Since Aug. 28, 2015 Views: 2273   Since Aug. 28, 2015
Yuri Ivanovich Khlopkov , Department of Aeromechanics and Flight Engineering, Moscow Institute of Physics and Technology, Zhukovsky, Russia.
Zay Yar Myo Myint , Department of Aeromechanics and Flight Engineering, Moscow Institute of Physics and Technology, Zhukovsky, Russia.
Anton Yurievich Khlopkov , Department of Aeromechanics and Flight Engineering, Moscow Institute of Physics and Technology, Zhukovsky, Russia.
Cognitive technology in computer science is combination of methods, algorithms and software for modeling the cognitive abilities of the human brain to solve specific application problems. The purposes of this paper are to describe the cognitive approaches in computer modeling systems and to create useful engineering program to predict aerothermodynamic characteristics of hypersonic aerospace vehicles in the all range of flow regimes.
Cognitive Technology, Aerospace Technology, Computer Modeling, Hypersonic Aerothermodynamics, Aerodynamics in Transitional Regime, Monte-Carlo
V. N. Gusev, “ High-altitude aerothermodynamics,” J. of Fluid Dynamics, Springer, 1993, Vol. 28, Issue 2, pp. 269-276.
G. I. Bagaev, G. P. Klemenkov and A. M. Kharitonov, “Problems of experimental study of supersonic flows”, Collection of Works, Dedicated to the Sixtieth Anniversary of the Academician V. V. Struminskiy, Nauka, Moscow, 1977.
Yu. I. Khlopkov, “Statistical Modeling in CFD” MIPT, Moscow, 2006. (in Russian)
O. M. Belotserkovskii and Yu. I. Khlopkov, “Monte Carlo Methods in Mechanics of Fluid and Gas,” World Scientific Publishing Co. N-Y, London, Singapore, Beijing, Hong Kong, 2010.
V.A. Perepukhov, “Application of the Monte-Carlo Method in the Dynamics of a Strongly Rarefied Gas, Collection of Works: Dynamics of Rarefied Gas and Molecular Gas Dynamics, Trudy TsAGI, Vol. 1411, 1972, pp. 54–72.
N. M. Kogan, “Rarefied Gas Dynamic,” New York, Plenum, 1969.
E. V. Alekseeva and R. G. Barantsev, “Local Method of Aerodynamic Calculation in a Rarefied Gas,” LGU, 1976.
V. S. Galkin, A. I. Erofeev and A. I. Tolstykh, “Approximate method of calculation of the aerodynamic characteristics of bodies in a hypersonic rarefied gas”, Proceedings TsAGI, Issue No. 1833, 1977, pp. 6-10. (in Russian)
Yu. I. Khlopkov, S. L. Chernyshev, Zay Yar Myo Myint and A. Yu. Khlopkov, “Introduction to specialty. High-speed aircraft vehicles,” MIPT, Moscow, 2013. (in Russian)
J.K. Haviland and M. D. Lavin, “Application of the Monte-Carlo Method to Heat Transfer in Rarefied Gases,” Phys. Fluids, Vol. 5, No. 1, 1962, pp. 279–286.
G. A. Bird, Molecular Gas Dynamics and the Direct Simulation of Gas Flows, Oxford University Press, 1994.
R. D. Neumann, “Missions and requirements. Special Course Aerothermodynamics of Hypersonic Vehicles,” AGARD Report 761, Neuilly sur Seine, France, 1988.
Zay Yar Myo Myint and A. Yu. Khlopkov, “Aerodynamic Characteristics of an Aircraft with a Complex Shape Taking into Account the Potential of Molecular Flow Interaction with a Surface,” TsAGI Science Journal, Vol. 41, No. 5, 2010, pp. 551-566. doi:10.1615/TsAGISciJ.v41.i5.50
Yu. I. Khlopkov, Zay Yar Myo Myint and A. Yu. Khlopkov, “Aerodynamic Investigation for Prospective Aerospace Vehicle in the Transitional Regime,” International Journal of Aeronautical and Space Sciences, KSAS, Korea, Vol. 14, No. 3, 2013, pp. 215-221.
Zay Yar Myo Myint, Yu. I. Khlopkov and A. Yu. Khlopkov, “Aerothermodynamics Investigation for Future Hypersonic Aerospace System,” 4th International Conference on Science and Engineering, Yangon, Myanmar, 9-10 December, 2013. (CD-ROM)
Yu. I. Khlopkov, V.A. Zharov, Zay Yar Myo Myint, and A.Yu. Khlopkov, “Aerodynamic Characteristics Calculation for New Generation Space Vehicle in Rarefied Gas Flow,” Universal Journal of Physics and Application, USA, Vol. 1, No. 3, 2013, pp. 286-289.
V. Kotov, E. Lychkin, A. Reshetin and A. Shelkonogov, “An Approximate Method of Aerodynamics Calculation of Complex Shape Bodies in a Transition Region,” Proc. of 13th International Conference on Rarefied Gas Dynamics, Plenum Press, New York, USA, Vol. 1, 1982, pp. 487–494.
Luigi Morsa, Gennaro Zuppardi, Antonio Schettino and Raffaele Votta, “Analysis of Bridging Formulae in Transitional Regime,” Proc. of 27th International Symposium on Rarefied Gas Dynamics, Pacific Grove, California, 10-15 July, 2010.
P. V. Vashchenkov, M. S. Ivanov and A.N. Krylov, “Numerical Simulations of High-Altitude Aerothermodynamics of a Promising Spacecraft Model,” Proc. of 27th International Symposium on Rarefied Gas Dynamics, Pacific Grove, California, 10-15 July, 2010, pp. 1337-1342.
V. Vaganov, S. Drozdov, A. P. Kosykh, G. G. Nersesov, I. F. Chelysheva and V. L. Yumashev, “Numerical Simulation of Aerodynamics of Winged Reentry Space Vehicle,” TsAGI Science Journal, Vol. 40, No. 2, 2009, pp. 131-149. doi:10.1615/TsAGISciJ.v40.i2.10
National Research Council. Review of NASA's Aerospace Technology Enterprise: An Assessment of NASA's Aeronautics Technology Programs. Washington, DC: The National Academies Press, 2004.
A. P. Kuleshov, A. V. Bernstein, “Advanced Multi-disciplinary Engineering Meta-modeling and Optimization Cognitive Information Technology for aerospace applications. International Aviation and Space Salon - 2009),” Moscow, Zhukovsky, August 19, 2009.
Open Science Scholarly Journals
Open Science is a peer-reviewed platform, the journals of which cover a wide range of academic disciplines and serve the world's research and scholarly communities. Upon acceptance, Open Science Journals will be immediately and permanently free for everyone to read and download.
Office Address:
228 Park Ave., S#45956, New York, NY 10003
Phone: +(001)(347)535 0661
Copyright © 2013-, Open Science Publishers - All Rights Reserved