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Engineering Methods to Calculate Heat Transfer Coefficients on the Surface Body in High-Speed Flow
Current Issue
Volume 6, 2019
Issue 1 (January)
Pages: 1-6   |   Vol. 6, No. 1, January 2019   |   Follow on         
Paper in PDF Downloads: 19   Since Apr. 9, 2019 Views: 894   Since Apr. 9, 2019
Authors
[1]
Zay Yar Myo Myint, Department of Aeromechanics and Flight Engineering, Moscow Institute of Physics and Technology, Zhukovsky, Russia.
[2]
Sergey Lvovich Gorelov, Department of Aeromechanics and Flight Engineering, Moscow Institute of Physics and Technology, Zhukovsky, Russia.
Abstract
The development of rocket and space technology is very important for any countries for two categories: construction high-speed passenger plane and reusable aerospace vehicle. It’s required continuous improvement of the research of processes of heat and mass transfer, and heat transfer theory development. Modeling research allows to quickly analysis the aerodynamic and heat exchange processes of high-speed aircrafts by using theoretical and experimental research. Well known method - Direct simulation Monte Carlo method (DSMC) is the basic quantitative tool for study of high-speed rarefied gas flow. These methods remain the most reliable approach, together with the local engineering methods, that provides good results for the global aerothermodynamics coefficients. Engineering methods are required small amount of computer resources (i.e. memory) and expensive at the initial stage of aircraft design and trajectory analysis. There are many engineering methods to calculate aerothermodynamics in hypersonic flow. In this paper described the analysis of the engineering methods to predict heat transfer coefficient on the surface of high-speed aircraft at high-altitude.
Keywords
High-Speed Aircraft, Bridging Methods, Transitional Flow Regime, Rarefied Gas Dynamics, Heat Transfer in Boundary Layer
Reference
[1]
N. M. Kogan, “Rarefied gas dynamic”, Plenum, 1969.
[2]
O. M. Belotserkovskii and Y. I. Khlopkov, “Monte Carlo Methods in Mechanics of Fluid and Gas,” World Scientific Publishing Co. New Jersy, London, Singapore, Beijing, Hong Kong, 2010.
[3]
E. H. Hirschel, “Basics of aerothermodynamics”. Progress in Astronautics and Aeronautics. AIAA, Springer-Verlag, Berlin/Heidelberg/New York, 2005.
[4]
G. A. Bird, “Molecular Gas Dynamics and the Direct Simulation of Gas Flows,” Oxford University Press, 1994.
[5]
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, 2013, Vol. 14, No. 3, pp. 215-221.
[6]
Zay Yar Myo Myint, Yu. I. Khlopkov and A. Yu. Khlopkov, “Aerothermodynamics Investigation for Future Hypersonic Aerospace Systems,” Proceedings of the 4th International Conference on Science and Engineering, Yangon, Myanmar, 9-10 December, 2013. (CD ROM).
[7]
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, 2013, Vol. 1, No. 3, pp. 286-289.
[8]
Yu. I. Khlopkov, Zay Yar Myo Myint, A. Yu., Khlopkov and M. S. Polyakov, “Computational analysis of aerodynamic characteristics for hypersonic vehicles”, International Journal of Applied and Fundamental Research, 2013, No. 2.
[9]
V. Kotov, E. Lychkin, A. Reshetin and A. Shelkonogov, “An Approximate method of aerodynamics calculation of complex shape bodies in a transition region”, In the proceeding of 13th International Conference on Rarefied Gas Dynamics, 1982, pp. 487–494.
[10]
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, 2010.
[11]
P. V. Vashchenkov, M. S. Ivanov and A. N. Krylov “Numerical simulations of high-altitude aerothermodynamics of a promising spacecraft model”, In the proceeding of 27th International Symposium on Rarefied Gas Dynamics, Pacific Grove, California, 2010, pp 1337-1342.
[12]
Yu. I. Khlopkov, S. L. Chernyshev, V. A. Zharov, Zay Yar Myo Myint, A. Yu. Khlopkov, M. S. Polyakov and Kyaw Zin, “Modern trends in the development of reusable aerospace system”, Asian Journal of Applied Sciences, 2014, Vol. 2, No. 1.
[13]
Yu. I. Khlopkov, S. L. Chernyshev, Zay Yar Myo Myint and A. Yu. Khlopkov, “Introduction to Speciality II. High-Speed Aircrafts,” Moscow, MIPT, 2013. (in Russian).
[14]
Zay Yar Myo Myint, Yu. I. Khlopkov and A. Yu. Khlopkov, “Aerothermodynamics Investigation for Future Hypersonic Aerospace Systems,” Proceedings of the 4th International Conference on Science and Engineering, Yangon, Myanmar, 9-10 December, 2013. (CD ROM).
[15]
Yu. I. Khlopkov, S. L. Chernyshev, Zay Yar Myo Myint, A. Yu. Khlopkov and A. A. Sorokina, “Notable Achievements in Aviation and Aerospace Technology”, Open Science Publishers, New York, 2015, 144 p.
[16]
S. L. Gorelov and Zeyar So “Self-similar interpolation in rarefied gas dynamics problems”, TsAGI Science Journal, 2010, No. 5, pp. 46-55.
[17]
G. Koppenwallner, B. Fritsche, T. Lips, H. Klinkrad, “Scarab-A Multi-disciplinary code for destruction analysis of space-craft during reentry”, Proceedings of the fifth european symposium on aerothermodynamics for space vehicles, 8-11 November 2005, Cologne, Germany.
[18]
Lee L., Laminar Heat Transfer over Blunt Nosed Bodies at Hypersonic Speeds. Jet Propulsion. Vol. 26, N. 4, pp. 259-269. 1956.
[19]
S. L. Gorelov “Physicochemical model of hypersonic flow around bodies with rarefied gas”, Journal Fluid Dynamics of Russian Academy of Sciences, 2002, №3. (in Russian).
[20]
G. Koppenwallner, B. Frittsche, T. Lips, “Aerodynamic and Aerothermal Analysis”, Tech. Report Hypersonic Technology: Int. Workshop on Astrodynamics Tools and Techniques, 2006, 35 p.
[21]
L. Lees, “Laminar Heat Transfer over Blunt nosed Bodies at Hypersonic Speeds”, Journal of Jet Propulsion, 1956, Vol. 26, No. 4, pp. 259-269.
[22]
P. V. Vashchenkov, “Numerical analysis of high altitude aerothermodynamics of space vehicles”, PhD thesis, Novosibirsk, 2012, 119 p. (in Russian).
[23]
Yu. I. Khlopkov, V. A. Zharov, Zay Yar Myo Myint and A. Yu. Khlopkov, “Investigation of the Heat Transfer Coefficients on the Body Surface in High-Speed Flow”, American Journal of Computer Science and Engineering, 2015, Vol. 2, No. 4, pp. 20-25.
[24]
V. Ya. Neiland, A. M. Tumin, “Aerodynamics of aerospace aircraft: Lecture notes”, Zhukovsky: FALT MIPT, 1991, 201 p.
[25]
Yu. I. Khlopkov, S. L. Chernyshev, Zay Yar Myo Myint and A. Yu. Khlopkov “The Use of Cognitive Approach to the Study of Aerothermodynamics of High-Speed Aircrafts”, MIPT press, Moscow, 2017, 194 p. (in Russian).
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