Abstract
The study continues the cycle of investigations concerned with the modeling of the methods of controlling flow regimes in compressible boundary layers. The effect of distributed heat and mass transfer on the stability parameters of a supersonic boundary layer is considered at amoderate supersonic Mach number M = 2. Emphasis is placed on the modeling of both the normal injection, when only the V component of the mean velocity is nonzero, and injection in other directions, including the tangential injection, when only the U component is nonzero on the wall. The formulation of the problem is similar with that of the gas curtain influence on the small fluctuation development. It is assumed that the effect of the injection of a similar gas with different temperatures is analogous to the injection of a gas with different densities, namely, the cold gas injection mimics the heavy gas injection, and vice versa. For this reason, in this study this modeling is realized by means of varying the temperature factor (wall heating or cooling). The case, in which the so-called “cutoff” regime is realized, that is, the velocity disturbances on a porous surface can be taken to be zero, is also considered.
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S.A. Gaponov and A.A. Maslov, “Stability of a Supersonic Boundary Layer with a Pressure Gradient and Suction,” in; Disturbance Development in Boundary Layers [in Russian], Novosibirsk (1979), p. 95.
S.A. Gaponov and N.M. Terekhova, “Stability and Three-Wave Interaction of Disturbances in a Supersonic Boundary Layer with Mass Transfer on the Wall,” Teplofiz. Aeromekh. 19, 301 (2012).
S.A. Gaponov and N.M. Terekhova, “Controlling Supersonic Boundary Layer Stability by Means of Distributed Mass Transfer through a PorousWall,” Fluid Dynamics 48 (6), 761 (2013).
A.V. Boiko, G.R. Grek, A.V. Dovgal’, and V.V. Kozlov, Turbulence Generation in Wall Flows [in Russian], Novosibirsk, Nauka (1999).
S.A. Gaponov and A.A. Maslov, Disturbance Development in Compressible Flows [in Russian], Novosibirsk, Nauka (1980).
E.P. Volchkov, Near-Wall Gas Curtains [in Russian], Novosibirsk, Nauka (1983).
M.V. Protasov, T.F. Ivanov, and A.F. Polyakov, “Distributed Injection Influence on Flow past a Blunt Body with a Permeable Leading Edge,” in: 11th Scientific and Technical Conf. on the Optical Methods of Flow Investigation [in Russian], Moscow (2011).
L.M. Albacete and W.J. Glowacki, “Skin Friction and Heat Transfer Characteristics of the Compressible Laminar Boundary Layer with Injection of a Light, Medium, and Heavy Gas,” NOLTR 66-215 (1967).
J.O. Powers, G. Heiche, and S.F. Shen, “The Stability of Selected Boundary-Layer Profiles,” NOLTR 62-143 (1963).
S.A. Gaponov and N.M. Terekhova, “Stability and Three-Wave Interaction of Disturbances in a Supersonic Boundary Layer with Cooling,” Vestn. NGU. Ser. Fizika 5 (3), 52 (2010).
S.A. Gaponov and N.M. Terekhova, “Controlling Supersonic Boundary Layer Stability by Means of Distributed Mass Transfer through a PorousWall,” Fluid Dynamics 48 (6), 761 (2013).
W.H. Dorrance, Viscous Hypersonic Flow, McGraw-Hill, New York (1962).
S.A. Gaponov and G.V. Petrov, Stability of the Boundary Layer of a Nonequilibrium Dissociating Gas [in Russian], Novosibirsk, Nauka (2013).
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Original Russian Text © S.A. Gaponov, N.M. Terekhova, 2016, published in Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, 2016, Vol. 51, No. 1, pp. 45–54.
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Gaponov, S.A., Terekhova, N.M. Joint effect of heat and mass transfer on the compressible boundary layer stability. Fluid Dyn 51, 45–55 (2016). https://doi.org/10.1134/S0015462816010063
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DOI: https://doi.org/10.1134/S0015462816010063