Yu. I. Khlopkov et al.

Acknowledgements

The support by RFBR (research project No. 11-07-00300-а) is cordially appreciated by the authors.

References

[1] Khlopkov, Yu . I., Chernyshev, S.L., Khlopkov, A.Yu. and Myint , Z.Y.M. (2013) Introduction to Specialt y. High-Speed

Aerial Vehicles. MIPT, Moscow.

[2] Koga n, N.M. (1969) Rarefied Gas Dynamic. P len um, New York. http://dx.doi.org/10.1007/978-1-4899 -6381-9

[3] Belo t serko vskii , O.M. and Khlopko v, Yu .I. (2010) Monte Carlo Methods in Mechanics of Fluid and Gas. World Scien-

tific Publishing Co. N-Y, London, Singapore, Beijing, Hong Kong.

[4] Gu s e v , V.N. (1993) High-Altitude Aerothermodynamics. Journal of Fluid Dynamics, 28, 269-276.

http://dx.doi.org/10.1007/BF01051218

[5] Neuman n, R.D. (19 88 ) Missions and Requi rements. Special Course Aerothermodynamics of Hypersonic Vehicles.

AGARD Report 761, Neuilly sur Seine, France.

[6] Hirsch el, E.H. (2005) Basics of Aerothermodynamics. Progress in Astronautics and Aeronautics, AIAA, Springer-

Verlag, Berlin/Heidelberg/New York.

[7] Bird, G. A. (1994) Molecular Gas Dynamics and the Direct Simulation of Gas Flows. Oxford University Press.

[8] Kotov, V., Lych ki n, E., Resheti n, A. and Shelkonogov, A. (1982) An Approximate Method of Aerodynamics Calcula-

tion of Complex Shape Bodies in a Transition Region. Proc. of 13th International Conference on Rarefied Gas Dy-

namics, Plenum Press, New York, 1, 487-494.

[9] Morsa, L., Zuppardi, G., Schettino, A. and Votta, R. (2010) Analysis of Bridging Formulae in Transitional Regime.

Proc. of 27th International Symposium on Rarefied Gas Dynamics, Pacific Grove, California, 10-15 July.

[10] Vashchenkov, P.V., Ivano v, M.S. and Kr ylov, A.N. (2010) Numerical Simulations of High-Altitude Aerothermody-

namics of a Promising Spacecraft Model. Proc. of 27th International Symposium on Rarefied Gas Dynamics, Pacific

Grove, California, 10-15 July, 1337-1342.

[11] Galki n, V.S., Er ofeev, A.I. and Tolstykh, A.I. (1977) Approximate Method of Calculation of the Aerodynamic Char-

acteristics of Bodies in a Hypersonic Rarefied Gas. Proceedings TsAG I , 18 33 , 6-10.

[12] Khlopkov, Yu. I. (2006) Statistical Modeling in CFD. MIPT, Moscow.

[13] M yin t, Z.Y.M. and Khlopkov, A.Yu. (2010 ) Aerodynamic Characteristics of an Aircraft with a Complex Shape Taking

into Account the Potential of Molecular Flow Interaction with a Surface. TsAGI Science Journal, 41, 551-566.

http://dx.doi.org/10.1615/TsAGISciJ.v41.i5.50

[14] Vagan ov, A.V., Drozdov, S., Kosykh, A.P., Nersesov, G.G., Chel yshe va, I.F. and Yumashev, V.L. (2009) Numerical

Simulation of Aerodynamics of Winged Reentry Space Vehicle. TsAGI Science Journal, 40, 131-149.

http://dx.doi.org/10.1615/TsAGISciJ.v40.i2.10

[15] Khlopkov, Yu.I., Myint, Z.Y.M. and Khlopkov, A.Yu. (2013) Aerodynamic Investigation for Prospective Aerospace

Vehicle in the Transitional Regime. International Journal of Aeronautical and Space Sciences, 14, 215-221.

http://dx.doi.org/10.5139/IJASS.2013.14.3.215

[16] M yin t, Z.Y.M., Khlopkov, Yu.I. and Khl opko v, A.Yu. (2013 ) Aerothermodynamics Investigation for Future Hyper-

sonic Aerospace Sys tem. Proc. of 4th International Conference on Science and Engineering, Yangon, Myanmar, 9-10

December.

[17] Khlopkov, Yu.I., Zharov, V.A., Myin t, Z.Y.M. and Khlopkov, A.Yu. (20 13 ) Aerodynamic Characteristics Calculation

for New Generation Space Vehicle in Rarefied Gas Flow. Universal Journal of Physics and Application, 1, 286-289.

[18] M yin t, Z.Y.M., Khlopkov, Yu.I., Khlopkov, A.Yu. and Polyakov , M.S. (2013) Computational Analysis of Aerod y-

namic Characteristics for Hypersonic Vehicles. International Journal of Applied and Fundamental Research.

[19] Khlopkov, Yu.I., Chernyshev, S.L., Zharov, V.A., Myint, Z.Y.M., Khlopkov, A.Yu., Polyakov, M.S. and Zin, K. (2014)

Modern Trends in the Development of Reusable Aerospace System. Asian Journal of Applied Sciences, 2.