NDLI: Joint effect of heat and mass transfer on the compressible boundary layer stability

Content Provider	Springer Nature Link
Author	Gapov, S. A. Terekhova, N. M.
Copyright Year	2016
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.
Starting Page	45
Ending Page	55
Page Count	11
File Format	PDF
ISSN	00154628
Journal	Fluid Dynamics
Volume Number	51
Issue Number	1
e-ISSN	15738507
Language	English
Publisher	Pleiades Publishing
Publisher Date	2016-03-23
Publisher Place	Moscow
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	compressible boundary layer hydrodynamic stability laminar-turbulent transition Fluid- and Aerodynamics Classical Continuum Physics Mechanics Engineering Fluid Dynamics
Content Type	Text
Resource Type	Article
Subject	Fluid Flow and Transfer Processes Physics and Astronomy Mechanical Engineering

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