Abstract
The effect of the temperature factor (body temperature ratio to the stagnation temperature of external flow) on the separated flow features has been investigated in the supersonic gas flow near the concave angle. The strong effect of the temperature factor on the separated zone length and on the corresponding aerodynamic performances was revealed. It was shown that, if the angle is big enough, such flow cannot be described by free interaction theory, i.e. by triple deck theory.
Access provided by Autonomous University of Puebla. Download to read the full chapter text
Chapter PDF
Similar content being viewed by others
References
Neiland, V. Ya., Kukanova, N. I., 1965, Investigation of flows with separation zones. Review of TsAGI, No. 129.
Lapin, Yu. V., Loytsianskii, L. G, Lun'kin, Yu. P., Neiland, V. Ya., Sychev, V. V., Tirskii, G. A., 1970, Mechanics of Viscous Liquids and Gases. Theory of Laminar and Turbulent Boundary Layers. Mechanics in USSR for Fifty Years. Vol. II, Nauka, Moscow.
Charwat, A. F., 1970, Supersonic Flows with Imbedded Separation Regions, in: Advances in Heat Transfer, Vol. 6. Academic, New York.
Chang, P. K., Separation of Flow. Pergamon, Oxford.
Chapman, D. R., 1951, An analysis of base pressure at supersonic velocities and comparison with experiment. NASA Rep., No 1051. pp. 23.
Korst, H. H., 1956, A theory for base pressure in transonic and supersonic flow. J. Appl. Mech., Vol. 23, No. 4, pp. 593–600.
Neiland, V. Ya., 1970, Asymptotic theory of plane steady supersonic flows with separation zones. Fluid Dynamics, No. 3, pp. 372.
Neiland, V. Ya., 1968, Supersonic viscous flow near a separation point. Abstracts of the 3-rd All-Union Congress on Theoretical and Applied Mathematics, Nauka, Moscow, pp. 224.
Neiland, V. Ya., 1969, Theory of laminar boundary layer separation in supersonic flow. Fluid Dynamics, No. 4, pp. 33.
Stewartson, K., Williams, P. G., 1969, Self-induced separation. Proc. Roy. Soc. London. Ser. A., Vol. 312, 1509, pp. 181–206.
Stewartson, K., 1970, On laminar boundary layers near corners//Quart J. Mech. Appl. Math., Vol. 23, No. 2. pp. 137–152.
Neiland, V. Ya., 1971, Flow behind the boundary layer separation point in a supersonic stream. Fluid Dynamics, No. 3, pp. 378.
Smith, F. T., Khorrami, A. F., 1991, The interactive breakdown in supersonic ramp flow. J. Fluid. Mech., Vol. 224, pp. 197–215.
Korolev, G. L., Gajjar, J. S. B., Ruban, A. I., 2002, Once again on the supersonic flow separation near a corner. J. Fluid Mech., Vol. 463, pp. 173–199.
Neiland, V. Ya., Bogolepov, V. V., Dudin, G. N., Lipatov, I. I., 2004, Asymptotic Theory of Supersonic Viscous Gas Flows. M.: Fizmatlit, pp. 456.
Neiland, V. Ya., Bogolepov, V. V., Dudin, G. N., Lipatov, I. I., 2007, Asymptotic Theory of Supersonic Viscous Gas Flows. Elsevier, Oxford, The Netherlands, pp. 536.
Hayes, W. D., and Probstein, R. F., 1959, Hypersonic Flow Theory. Academic, New York.
Egorov, I. V., Zaitsev, O. L., 1991, On an approach to the numerical solution of the two-dimensional Navier-Stokes equations by the shock capturing method. Journal of Computational Mathematics and Mathematical Physics. Vol. 31, No 2. pp. 286–299.
Babaev, I. Yu., Bashkin, V. A., Egorov, I. V., 1994, Numerical solution of the Navier-Stokes equations using variational iteration methods. Comp. Maths Math Phys., Vol. 34, No 11. pp. 1455–1462.
Bashkin, V. A., Egorov, I. V., Ivanov, D. V., 1997, Application of Newton's method to the calculation of internal supersonic separated flows. Zh. Prikl. Mekh. Tekhn. Fiz., Vol. 38, No 1, pp. 30–42.
Godunov, S. K., 1959, Mat. Sb., Vol. 47, pp. 271.
Roe, P. L., 1981, Aproximate Rieman Solvers, Parameter Vectors, and Difference Scheme. Journal Computation Physics, Vol. 43, pp. 357–372.
Kolgan, V. P., 1972, Uch. Zap. Tsentr. Aerogidrodin. Inst., Vol. 3, No. 6, pp. 68.
Saad, Y., Shultz, M. H., 1986, GMRES: a generalized minimal residual algorithm for solving nonsymmetric linear systems. SIAM Journal of Scientific and Statistical Computing, No. 7, pp. 856–869.
Gil'manov, A. N., 2000, Methods of Adaptive Meshes in Gas Dynamic Problems, I. Nauka, Fizmatlit, Moscow, pp. 247.
Anderson, D. A., Tannehill, J. C., Pletcher, R. H., 1984, Computational Fluid Mechanics And Heat Transfer. Hemisphere, New York.
Stemmer, C., Adams, N. A., 2004, Investigation of supersonic boundary layers by DNS, ECCOMAS 2004 Proceedings, Vol. II.
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2009 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Neyland, V.Y., Sokolov, L.A., Shvedchenko, V.V. (2009). Temperature Factor Effect on Separated Flow Features in Supersonic Gas Flow. In: Hegarty, A., Kopteva, N., O'Riordan, E., Stynes, M. (eds) BAIL 2008 - Boundary and Interior Layers. Lecture Notes in Computational Science and Engineering, vol 69. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-00605-0_3
Download citation
DOI: https://doi.org/10.1007/978-3-642-00605-0_3
Published:
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-00604-3
Online ISBN: 978-3-642-00605-0
eBook Packages: Mathematics and StatisticsMathematics and Statistics (R0)