Skip to main content
Log in

Investigations on controlled transition development in a laminar separation bubble by means of LDA and PIV

  • Original Paper
  • Published:
Experiments in Fluids Aims and scope Submit manuscript

Abstract

When a laminar boundary layer separates because of an adverse streamwise pressure gradient, the flow is subject to increased instability with respect to small-amplitude disturbances. Laminar–turbulent transition occurs under a rapid three-dimensional (3D) development within the separated shear layer. When the following turbulent boundary layer reattaches, a laminar separation bubble is formed. To allow controlled measurements, a small-amplitude Tollmien–Schlichting wave (TS wave) was introduced into the boundary layer without (case I) and with (case II) spanwise forcing of steady 3D disturbances. Combined application of laser-Doppler anemometry (LDA) and particle image velocimetry (PIV) demonstrates the suitability of both measurement techniques to capture the development of unsteady, periodic phenomena. The transition mechanism occurring in the flow field under consideration is discussed, and results obtained by controlled measurements are compared to direct numerical simulations (DNS) and predictions from linear stability theory (LST). Flow visualizations and stereoscopic PIV measurements give better insight into the 3D breakdown of the separated shear layer.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Fig. 1.
Fig. 2.
Fig. 3.
Fig. 4.
Fig. 5.
Fig. 6.
Fig. 7.
Fig. 8.
Fig. 9.
Fig. 10.
Fig. 11.
Fig. 12.
Fig. 13.
Fig. 14.
Fig. 15.
Fig. 16.
Fig. 17.
Fig. 18.
Fig. 19.

Similar content being viewed by others

Abbreviations

a :

amplitude

f 0 :

fundamental frequency

H 12 :

boundary layer shape factor, H 12=δ 1/δ 2

h :

wavenumber coefficient in time

k :

wavenumber coefficient in the spanwise direction

l :

liter

m :

meter

Re x :

Reynolds number based on streamwise distance of the leading edge

Re δ1 :

Reynolds number based on the displacement thickness δ 1

s :

second

t :

time

u :

freestream velocity

u δ :

velocity at the boundary layer edge

u,v,w :

velocities

u′,v′:

velocity fluctuations

x :

streamwise coordinate

y :

wall-normal coordinate

z :

spanwise coordinate

δ :

boundary layer thickness

δ 1 :

boundary layer displacement thickness

δ 2 :

boundary layer momentum thickness

λ z :

spanwise wavelength

Φ :

phase angle

References

  • Alam M, Sandham ND (2000) Direct numerical simulation of 'short' laminar separation bubbles with turbulent reattachment. J Fluid Mech 410:1–28

    Article  CAS  Google Scholar 

  • Boiko AV, Grek GR, Dovgal AV, Koslov VV (2002) The origin of turbulance in near-wall flows. Springer, Berlin Heidelberg New York

  • Briley WR (1971) A numerical study of laminar separation bubbles using the Navier–Stokes equations. J Fluid Mech 47:713–736

    Google Scholar 

  • Fitzgerald EJ, Mueller TJ (1988) Measurements in a separation bubble on an airfoil using laser velocimetry. AIAA J 28:584–592

    Google Scholar 

  • Gaster M (1966) The structure and behavior of laminar separation bubbles. AGARD CP 4:813–854

    Google Scholar 

  • Klebanoff PS, Tidstrom KD, Sargent LM (1962) The three-dimensional nature of boundary layer instability. J Fluid Mech 12:1–41

    Google Scholar 

  • Kruse M, Wagner S (1996) Measurements of laminar–turbulent transition in a flat-plate boundary layer. In: Proceedings of the 8th international symposium of laser techniques to fluid mechanics, Lisbon, 8–11 July

  • Kruse M (1997) Einsatz der Laser-Doppler-Anemometrie zur Untersuchung des laminar-turbulenten Grenzschichtumschlags an der ebenen Platte. Dissertation, University of Stuttgart, Germany

  • Lang M, Marxen O, Rist U, Wagner S (2000a) Experimental and numerical investigations on transition in a laminar separation bubble. In: Wagner S et al. (eds) Notes on numerical fluid mechanics, new results in numerical and experimental fluid mechanics. Springer, Berlin Heidelberg New York

  • Lang M, Marxen O, Rist U, Wagner S (2000b) LDA-Messungen zur Transition in einer laminaren Ablöseblase. In: Proceedings of 8th Fachtagung der GALA, Lasermethoden in der Strömungsmesstechnik, Freising-Weihenstephan, Germany, 12–14 Sept. Shaker, Aachen

  • Marxen O, Lang M, Rist U, Wagner S (2002) A combined experimental/numerical study of unsteady phenomena in a laminar separation bubble. In: Proceedings of IUTAM symposium "unsteady separated" flows, Toulouse (available on CD-ROM)

  • Marxen O, Rist U,Wagner S (2003) The effect of spanwise-modulated disturbances on transition in a 2-D separated boundary layer. AIAA paper no. 2003-0789

  • Maucher U, Rist U, Wagner S (1999) Transitional structures in a laminar separation bubble. In: Nitsche W, Heinemann R, Hilbig HJ (eds.) Notes on numerical fluid mechanics, new results in numerical and experimental fluid mechanics. Vieweg, Wiesbaden

  • Rist U (2002) On instability and transition in laminar separation bubbles. In: Proceedings of CEAS aerospace aerodynamics research conference, Cambridge, UK, 10–12 June 2002, (available on CD-ROM)

  • Rist U (1998) Zur Instabilität und Transition in laminaren Ablöseblasen. Habilitation, Universität Stuttgart, Shaker, Aachen

  • Rist U, Augustin K, Wagner S (2000) Numerical simulation of laminar separation-bubble control. In: Wagner S et al. (eds) Notes on numerical fluid mechanics, new results in numerical and experimental fluid mechanics. Springer, Berlin Heidelberg New York

  • Ronneberger O, Raffel M, Kompenhans J (1998) Advanced evaluation algorithms for standard and dual plane particle image velocimetry. In: Proceedings of 9th international symposium of laser techniques to fluid mechanics, Lisbon, 13–16 July

  • Spalart PR, Strelets MK (2000) Mechanisms of transition and heat transfer in a separation bubble. J Fluid Mech 403:329–349

    Article  Google Scholar 

  • Strunz M, Speth JF (1987) A new laminar water-tunnel to study the transition process in a Blasius boundary layer and in a separation bubble and a new tool for industrial aerodynamics and hydrodynamic research. AGARD CP 413:25-1– 25-5

    Google Scholar 

  • Watmuff J (1999) Evolution of a wave packet into vortex loops in a laminar separation bubble. J Fluid Mech 397:119–169

    Article  Google Scholar 

  • Westerweel J, van Oord J (2000) Stereoscopic PIV measurements in a turbulent boundary layer. In: Stanislas M, Kompenhans J, Westerweel J (eds) Particle image velocimetry, progress toward industrial application. Kluwer, Dordrecht

  • Wiegand T (1997) Experimentelle Untersuchungen zum laminar-turbulenten Transitionsprozess eines Wellenzuges in einer Plattengrenzschicht. Dissertation, University of Stuttgart, Germany

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to M. Lang.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Lang, M., Rist, U. & Wagner, S. Investigations on controlled transition development in a laminar separation bubble by means of LDA and PIV . Exp Fluids 36, 43–52 (2004). https://doi.org/10.1007/s00348-003-0625-x

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s00348-003-0625-x

Keywords

Navigation