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Passive Control of Shock/Boundary Layer Interaction

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Control of Flow Instabilities and Unsteady Flows

Part of the book series: International Centre for Mechanical Sciences ((CISM,volume 369))

Summary

Normal shock wave — turbulent boundary layer phenomena are presented and discussed. Examples of experimental results are set up to provide a convincing material about the interaction field structure and its behaviour under the influence of key parameters. Besides, various theoretical approaches are presented and explained, the historical as well as the modern ones. A comparison of the theoretical results with corresponding experiments illustrates the abilities of applied methods. Finally, the material presented here, describes some of the modifications being introduced to standard passive control in order to improve the effectiveness of ventilation.

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Abbreviations

c:

chord length

cD :

drag coefficient

cDv :

viscous drag coefficient

cDw :

wave drag coefficient

cf :

friction coefficient

cl :

lift coefficient

cp :

pressure coefficient

c*:

critical velocity of sound

M:

Mach number

Mδ :

Pre-shock Mach number

M *0 (y):

critical Mach number profil of the upstream undisturbed boundary layer

p:

static pressure

Pr:

Prandtl number

R:

Radius of wall curvature

Re:

Reynolds number

u , v:

mean flow velocity components

x , y:

Cartesian coordinates

y0 :

thickness of the viscous sublayer

α:

angle of attack

β:

exponent of the velocity profil in the boundary layer

δ:

boundary layer thickness

δ1 :

displacement thickness

δ2 :

momentum thickness

κ:

ratio of constant specific heats

λ:

coefficient of thermal conduction

λn :

eigenvalues

μ:

dynamic viscosity

ν:

kinematic viscosity

ρ:

density

τw :

wall shear stress

I:

Subscripts and Superscripts

G:

undisturbed basic flow

n , t:

normal, tangential

s:

disturbance quantity

w:

wall

~:

dimensional quantities

*:

critical

∞:

free stream conditions

References

  1. Bahi, L., Ross, J.M. and Nagamatsu, H.T.: Passive shock wave/boundary layer control for transonic airfoil drag reduction. AIAA-Paper 83 - 0137 (1983)

    Google Scholar 

  2. Thiede, P., Krogmann, P. and Stanewsky, E.: Active and passive shock-boundary layer interaction control on supercritical airfoils. AGARD-CP-365, Brussels 1984

    Google Scholar 

  3. Krogmann, P., Stanewsky, E. and Thiede, P.: Transonic shock/boundary layer interaction control. ICAS-Paper 84-2.3.3, Toulouse 1984

    Google Scholar 

  4. Bohning, R. and Zierep, J.: Calculation of 2D Turbulent Shock/Boundary-Layer Interaction at Curved Surface with Suction and Blowing. In: Turbulent Shear Layer/Shock Wave Interactions, IUTAM Symposium Palaiseau 1985 (ed: J. Délery ), Springer-Verlag 1985, pp 105 - 112

    Google Scholar 

  5. Bohning, R. and Jungbluth, H.: Turbulent Shock/Boundary Layer Interaction with Control. In: Symposium Transsonicum Ill (ed: J. Zierep and H. Oertel jr.), Springer-Verlag Berlin 1989, pp. 389 - 398

    Google Scholar 

  6. Breitling, T.: Berechnung transsonischer, reibungsbehafteter Kanal-und Profilströmungen mit passiver Beeinflussung. Dissertation, Universität Karlsruhe 1989

    Google Scholar 

  7. Braun, W.: Experimentelle Untersuchung der turbulenten Stoß-Grenzschicht-Wechselwirkung mit passiver Beeinflussung. Dissertation, Universität Karlsruhe 1990

    Google Scholar 

  8. Délery, J., Chanetz, B. and Pot, T.: Fundamental Experiments on Passive Control Applied to Transonic Shock-Wave/Boundary-Layer Interaction. In: 3. STAB-Workshop, Nov. 10-11, 1987, DFVLR Göttingen

    Google Scholar 

  9. Raghunathan, S. and Mabey, D.G.: Passive shock wave/boundary-layer control on a wall-mounted model. AIAA-Journal 25 (1987), 275ff

    Google Scholar 

  10. Liu, X. and Squire, L.C.: An investigation of shock-boundary-layer interactions on curved surfaces at transonic speeds. J. Fluid Mech. 187 (1988), 467 - 468

    Article  Google Scholar 

  11. Dargel, G. and Thiede, P.: Viscous transonic airfoil flow simulation by an efficient viscous-inviscid interaction method. AIAA-Paper 87 - 0412 (1987)

    Google Scholar 

  12. Délery, J., Bur, R. and Pot, T.: Basic experiments on passive control of shockwave/boundary-layer interaction in transonic flow. In: 4. STAB-Workshop 1989, DLR Göttingen

    Google Scholar 

  13. Bohning, R. and Zierep, J.: Der senkrechte Verdichtungstoß an der gekrümmten Wand unter Berücksichtigung der Reibung. ZAMP 27 (1976), 225 - 240

    Article  MATH  Google Scholar 

  14. Bohning, R. and Zierep, J.: Normal Shock-Turbulent Boundary Layer Interaction at a Curved Wall. AGARD CP No. 291, Computation of viscous-inviscid interactions (1980), pp 17-1-17-8

    Google Scholar 

  15. Bohning, R.: Die Wechselwirkung eines senkrechten Verdichtungsstoßes mit einer turbulenten Grenzschicht an einer gekrümmten Wand. Habilitationsschrift, Universität Karlsruhe 1982

    Google Scholar 

  16. Lighthill, M.J.: On Boundary Layers and Upstream Influence, II. Supersonic Flow Without Separation. Proc. Royal Soc., A 217 No. 1131 (1953), 478 - 507

    Article  Google Scholar 

  17. Ackeret, J., Feldmann, F. and Rott, N.: Untersuchungen an Verdichtungsstößen und Grenzschichten in schnell bewegten Gasen. Mitteilungen aus dem Institut für Aerodynamik, ETH Zürich, No. 10, 1946

    Google Scholar 

  18. Oswatitsch, K. and Zierep, J.: Das Problem des senkrechten Stoßes an einer gekrümmten Wand. ZAMM 40 (1960), 143-144 (Tagungsheft)

    Google Scholar 

  19. Beam, R.M. and Warming, R.F.: An implicit factored scheme forthe compressible Navier-Stokes equations. AIAA Journal 16 (1978), 393 - 402

    Article  MATH  Google Scholar 

  20. Chen, C.L.: Computation of transonic flow over porous airfoils. Ph.D. Thesis, University of Colorado 1986

    Google Scholar 

  21. Carter, J.E.: A new boundary layer inviscid iteration technique for separated flow. AIAA Paper 79 - 1450 (1979)

    Google Scholar 

  22. Le Balleur, J.C.: Strong maching method for computing for transonic viscous flows including wakes and separations. Lifting airfoils. La Recherche Aerospatiale 1981-3 (1981), pp. 21 - 45

    Google Scholar 

  23. Bohning, R., Thiede, P. and Dargel, G.: Numerical simulation of viscous transonic airfoil flows with passive shock control. In: Acta Mechanica (1994) Suppl. 4, Fluid and Gasdynamics (ed: G. Schnerr, R. Bohning, K. Bühler, W. Frank), Springer-Verlag Wien, New York, pp. 219 - 231

    Google Scholar 

  24. Bohning, R. and Zierep, J.: Turbulent Shock-Boundary-Layer Interaction with Passive Control by Normal Suction and Normal Tangential Blowing. Proceedings of the 2nd International Conference on Fluid Mechanics (ICFM II). Beijing 1993, Peking University Press, China, pp. 253 - 258

    Google Scholar 

  25. Bohning, R. and Liang D.W.: Internal report

    Google Scholar 

  26. Bohning, R. and Doerffer, P.: Investigation of Porous Plate Flow. Karlsruhe, internal report (1994), will be published.

    Google Scholar 

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Author information

Authors and Affiliations

  1. University of Karlsruhe (TH), Karlsruhe, Germany

    R. Bohning

Authors
  1. R. Bohning
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Editor information

Editors and Affiliations

  1. DLR Institute for Fluid Mechanics, Germany

    G. E. A. Meier

  2. University of Karlsruhe, Germany

    G. H. Schnerr

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© 1996 Springer-Verlag Wien

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Bohning, R. (1996). Passive Control of Shock/Boundary Layer Interaction. In: Meier, G.E.A., Schnerr, G.H. (eds) Control of Flow Instabilities and Unsteady Flows. International Centre for Mechanical Sciences, vol 369. Springer, Vienna. https://doi.org/10.1007/978-3-7091-2688-2_6

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  • DOI: https://doi.org/10.1007/978-3-7091-2688-2_6

  • Publisher Name: Springer, Vienna

  • Print ISBN: 978-3-211-82807-6

  • Online ISBN: 978-3-7091-2688-2

  • eBook Packages: Springer Book Archive

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