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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 />

✬<br />

✫<br />

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 />

1. Morkovin M.V. Critical evaluation <strong>of</strong> transition from laminar to turbulent shear layer with<br />

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 />

4. Gaponov S.A. On the interaction <strong>of</strong> a supersonic bo<strong>und</strong>ary layer with acoustic disturbances.<br />

Thermophysics and Aeromechanics, Vol.2, №3, 1995, pp.181-188.<br />

5. Fedorov A.V., Hohlov A.P. Excitation <strong>of</strong> unstable modes in a supersonic bo<strong>und</strong>ary layer by<br />

acoustic waves. Fluid Dynamics, №4, 1991, pp.67-71 (in Russian).<br />

6. Semionov N.V., Kosinov A.D., Maslov A.A. Experimental investigation <strong>of</strong> supersonic bo<strong>und</strong>ary<br />

layer receptivity. Transitional bo<strong>und</strong>ary layers in aeronautics, edited by R.A.W.M.Henkes and<br />

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 />

✩<br />

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