BAIL 2006 Book of Abstracts - Institut für Numerische und ...
BAIL 2006 Book of Abstracts - Institut für Numerische und ...
BAIL 2006 Book of Abstracts - Institut für Numerische und ...
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S.A. GAPONOV, G.V. PETROV, B.V. SMORODSKY: Bo<strong>und</strong>ary layer intercation with<br />
external disturbances<br />
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M where M = M cos χ and<br />
disturbance amplitude takes place for oblique roughness at = 1<br />
χ is the angle between the roughness wave front and the plate leading edge. At the BL outer edge the<br />
disturbance amplitude is almost zero because it is already damped inside the BL. The problem <strong>of</strong><br />
nonlinear interactions <strong>of</strong> the disturbances induced by so<strong>und</strong> and roughness was investigated. It has<br />
been fo<strong>und</strong> that the parameter, which defines the ability to the instability wave excitation (receptivity<br />
coefficient) is strongly dependent <strong>of</strong> the acoustics incidence angle and the roughness wave front<br />
orientation. Computations show that even at high subsonic external flow velocities the receptivity is<br />
strongly dependent also on the direction <strong>of</strong> so<strong>und</strong> propagation. At M > 1 the instability could be<br />
excited by disturbances with the wavelength much smaller than TS wave wavelength. Maximal<br />
receptivity corresponds to the case when the angle between the roughness wave front and the mean<br />
flow is close to the Mach angle.<br />
The paper presents results <strong>of</strong> the detailed investigation <strong>of</strong> the interaction <strong>of</strong> supersonic BL with<br />
external vortical and thermal perturbations. The bo<strong>und</strong>ary conditions for the disturbance at the BL<br />
outer edge are <strong>und</strong>er special consideration. It has been fo<strong>und</strong> that inside the BL the streamwise<br />
velocity and mass flux perturbations can exceed much the amplitude <strong>of</strong> the external vorticity waves.<br />
The disturbance excitation rate is reducing with increasing Mach number. The influence <strong>of</strong> the<br />
external thermal wave onto the flow inside the BL is considerably The results <strong>of</strong> the computations <strong>of</strong><br />
the intensity and the spatial dimensions <strong>of</strong> the streamwise streaky structures in the BL are in<br />
agreement with measurements [9].<br />
This work has been performed <strong>und</strong>er the financial support <strong>of</strong> RFBR and the Russian Federation<br />
President Council (projects 05-01-00079-a, NSh-9642003.1).<br />
References<br />
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emphasis on hypersonically trevelling bodies. Tech. Rep. AFFDL № 68-149, 1969.<br />
2. Kachanov Yu.S. Physical mechanisms <strong>of</strong> laminar-bo<strong>und</strong>ary-layer transition. Annu.Rev.Fluid<br />
Mech., Vol.26, 1994, p.411.<br />
3. Boyko A.V., Greek G.R., Dovgal A.V., Kozlov V.V. Turbulence origin in near-wall flows.<br />
Novosibirsk: Science, 1999 (in Russian).<br />
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Thermophysics and Aeromechanics, Vol.2, №3, 1995, pp.181-188.<br />
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J.L. van Ingen. North-Holland, Amsterdam, 1996, pp.413-420.<br />
7. Kovasznay L.S.G. Turbulence in supersonic flow. J.Aeron.Sci., Vol.20, №10, 1953, pp.657-674.<br />
8. Petrov G.V. New parabolized system <strong>of</strong> equations <strong>of</strong> stability <strong>of</strong> a compressible bo<strong>und</strong>ary<br />
layer. J. Appl.Mech. Techn. Phys. Vol.41, №1, 2000, p. 55-61.<br />
9. Westin K.J.A., BakchinovA.A., Kozlov V.V., Alfredsson P.H. Experiments on localized<br />
disturbances in a flat plate bo<strong>und</strong>ary layer. Pt 1: The receptivity and evolution <strong>of</strong> a localized free<br />
stream disturbances. Europ. J. Mech., B. Fluids, Vol.17, №6, 1998, pp.823-846.<br />
Speaker: GAPONOV, S.A. 86 <strong>BAIL</strong> <strong>2006</strong><br />
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