Skip to main content
Log in

Control of low-speed turbulent separated flow using jet vortex generators

  • Originals
  • Published:
Experiments in Fluids Aims and scope Submit manuscript

Abstract

A parametric study has been performed with jet vortex generators to determine their effectiveness in controlling flow separation associated with low-speed turbulent flow over a two-dimensional rearward-facing ramp. Results indicate that flow-separation control can be accomplished, with the level of control achieved being a function of jet speed, jet orientation (with respect to the free-stream direction), and jet location (distance from the separation region in the free-stream direction). Compared to slot blowing, jet vortex generators can provide an equivalent level of flow control over a larger spanwise region (for constant jet flow area and speed).

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.

Similar content being viewed by others

Abbreviations

C p :

pressure coefficient, 2(P-P∞)/ϱV 2

C Q :

total flow coefficient, Q/δ λ v

D 0 :

jet orifice diameter

Q :

total volumetric flow rate

R θ :

Reynolds number based on momentum thickness

u′ :

fluctuating velocity component in the free-stream (x) direction

V :

free-stream flow speed

VR :

ratio of jet speed to free-stream flow speed

x :

coordinate along the wall in the free-stream direction

α :

jet inclination angle (angle between the jet axis and the wall)

β :

jet azimuthal angle (angle between the jet axis and the free-stream direction in a horizontal plane)

δ :

boundary-layer thickness

θ :

momentum thickness

λ :

lateral distance between jet orifices

References

  • Bertin, J.; Smith, M. 1989: Aerodynamics for engineers. Englewood Cliffs, New Jersey: Prentice Hall

    Google Scholar 

  • Compton, D.; Johnston, J. 1991: Streamwise vortex production by pitched and skewed jets in a turbulent boundary layer. AIAA Paper 91-0038

  • Johnston, J.; Nishi, M. 1990: Vortex generator jets — means for flow separation control. AIAA J. 28, 989–994

    Google Scholar 

  • Lin, J.; Howard, F.; Selby, G. 1989: Turbulent flow separation control through passive techniques. AIAA Paper 89-0976

  • Lin, J.; Howard, F.; Selby, G. 1990: Experimental investigation of several passive and active methods for turbulent flow separation control. AIAA Paper 90-1598

  • Olason, M.; Norton, D. 1966: Aerodynamic design philosophy of the boeing 737. J. Aircraft 3, 524–528

    Google Scholar 

  • Papell, S. 1984: Vortex generating flow passage design for increased film-cooling effectiveness and surface coverage. NASA TM 83617

  • Pearcey, H.; Stuart, C. 1959: Methods of boundary-layer control for postponing and alleviating buffeting and other effects of shock-induced separation. SMF Paper No. FF-22. New York: Institute of the Aeronautical Sciences

    Google Scholar 

  • Rao, D.; Kariya, T. 1988: Boundary-layer submerged vortex generators for separation control — an exploratory study. AIAA Paper No. 88-3546-CP

  • Selby, G. 1989: Passive control of three-dimensional separated vortical flow associated with swept rearward-facing steps. J. Fluids Eng. 11, 99–101

    Google Scholar 

  • Wallis, R. 1952: The use of air jets for boundary-layer control. Aerodynamics Research Laboratories (Australia), Aero Note 110

    Google Scholar 

  • Wheeler, G. 1984: Means of maintaining attached flow of a flow medium. U.S. Patent No. 4455045

  • Zhang, S.; Li, F. 1987: Experiments about the air jet vortex generator. Proc. of the 8th Institute of Aeronautics and Astronautics, Cincinnati, Ohio, 513–516

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

About this article

Cite this article

Selby, G.V., Lin, J.C. & Howard, F.G. Control of low-speed turbulent separated flow using jet vortex generators. Experiments in Fluids 12, 394–400 (1992). https://doi.org/10.1007/BF00193886

Download citation

  • Received:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF00193886

Keywords

Navigation