Investigation of the Heat Transfer Coefficients on the Body Surface in High Speed Flow
[1]
Yuri Ivanovich Khlopkov, Department of Aeromechanics and Flight Engineering, Moscow Institute of Physics and Technology, Zhukovsky, Russia.
[2]
Vladimir Alekseevich Zharov, Department of Aeromechanics and Flight Engineering, Moscow Institute of Physics and Technology, Zhukovsky, Russia.
[3]
Zay Yar Myo Myint, Department of Aeromechanics and Flight Engineering, Moscow Institute of Physics and Technology, Zhukovsky, Russia.
[4]
Anton Yurievich Khlopkov, Department of Aeromechanics and Flight Engineering, Moscow Institute of Physics and Technology, Zhukovsky, Russia.
The development of high speed aircraft technology requires continuous improvement of the research processes of heat exchange on the surface of the aircraft. In this paper present the methods for calculating the heat transfer coefficients on surface of high-speed aircrafts. The effective length method is suitable to calculate convective heat transfer on surface body in laminar and turbulent boundary layer at high-speed flows. The engineering methods to calculate heat transfer coefficients on the surface of aircrafts in hypersonic flows are also presented.
Effective Length Method, Boundary Layer, High-Speed Aerodynamics, The Convective Heat Flux, Local-bridging Method
[1]
John D. Anderson, “Hypersonic and High Temperature Gas Dynamics,” McGraw-Hill, New York, 1989.
[2]
Jack J. McNamara, Peretz P. Friedmann, Kenneth G. Powell, and Biju J. Thuruthimattam, “Aeroelastic and Aerothermoelastic Behavior in Hypersonic Flow,” AIAA Journal, Vol. 46, No. 10, 2008, pp. 2591-2610.
[3]
J. J. Bertin, “Hypersonic Aerothermodynamics,” AIAA Education Series, Washington D.C., 1994.
[4]
L.F. Crabtree, R.L. Dommett and J.G. Woodley, R.A.E. Farnborough, “Estimation of Heat Transfer to Flat Plates, Cones and Blunt Bodies,” London, Reports and Memoranda, No. 3637, 1965.
[5]
James F. Schmidt, “Turbulent skin-friction and heat-transfer coefficients for an inclined flat plate at high hypersonic speeds in terms of free-stream flow properties,” United States. NASA, 1961.
[6]
W. F. N. Santos, “Leading-edge bluntness effects on aerodynamic heating and drag of power law body in low-density hypersonic flow,” Journal of the Brazilian Society of Mechanical Sciences and Engineering, Vol. 27, No. 3, 2005.
[7]
S. Saravanan, G. Jagadeesh and K.P.J. Reddy, “Convective heat-transfer rate distributions over a missile shaped body flying at hypersonic speeds,” Experimental Thermal and Fluid Science, Vol. 33, No. 4, 2009, pp. 782–790.
[8]
G. K. Mikhailov and V.Z. Parton, “Super- and hypersonic aerodynamics and heat transfer,” CRC press, United States, 1993.
[9]
J. O. Reller Jr., “Heat Transfer to Blunt Nose Shapes with Laminar Boundary Layers at High Supersonic Speeds,” NACA RM-A57FO3a, 1957.
[10]
V. S. Avduyevskii, “Fundamentals of heat transfer in aviation and rocket and space technology,” Moscow, Mechanical Engineering, 1992. (in Russian)
[11]
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.
[12]
N. M. Kogan, “Rarefied Gas Dynamic,” New York, Plenum, 1969.
[13]
V. N. Gusev, “ High-altitude aerothermodynamics,” J. of Fluid Dynamics, Springer, 1993, Vol. 28, Issue 2, pp. 269-276.
[14]
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.
[15]
Yu. I. Khlopkov, S. L. Chernyshev, Zay Yar Myo Myint and A. Yu. Khlopkov, “Introduction to specialty II. High-speed aircrafts,” MIPT, Moscow, 2013. (in Russian)
[16]
Yu.I. Khlopkov, S.L.Chernyshev, Zay Yar Myo Myint and A.Yu. Khlopkov, “Hypersonic aerothermodynamic investigation for aerospace system,” Proceeding of 29th congress of the international council of the aeronautical sciences, St. Petersburg, September 7-12, 2014. (USB)
[17]
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.
[18]
Richard D. DeLauer, “Experimental heat transfer at hypersonic mach number,” Dissertation (Ph.D.), California Institute of Technology, 1953. http://resolver.caltech.edu/CaltechETD:etd-04222003-111626
[19]
S.V. Zhurin, “The technique of numerical modeling of convective heat the bodies of complex shape using the method the effective length,” Dissertation (Ph.D.), Moscow Institute of Physics and Technology, 2009. (in Russian)
[20]
Zay Yar Myo Myint and A. Y. Khlopkov, “Calculation method of heat flows in laminar and turbulent boundary layer,” Proceedings of the 56th scientific conference of MIPT “Actual problems of fundamental and applied sciences in the modern information society" and “All-Russian Youth Research and Innovation Conference”, Zhukovsky, 2013, pp. 28-29. (in Russian)
[21]
V. P. Solncev, B. M. Galitseisky, B. M. Glebov, B. M. Kalmyks, I. I. Shkarban and A. E. Pirogov, “Methodological guidelines for settlement and graphic works: heat transfer on the surface of aircraft,” Moscow, MAI, 1987. (in Russian)
[22]
P. V. Vashchenkov, “Numerical analysis of high-altitude spacecraft aerothermodynamics,” PhD thesis, Novosibirsk, ITAM SB RAS, 2012.
