MetaCartSign in to MyCiteSeer

Include Citations | Advanced Search | Help

Include Citations | Advanced Search | Help

  y

Download:
Download as a PDF | Download as a PS
by Flow Over, A Stratford Ramp, H. L. Zhang, H. F. Fasel
http://cfd.ame.arizona.edu/~hui/ps/reno99.ps.gz
Add To MetaCart

Abstract:

The applicability of flow control by periodic blowing and suction through a slot in a spatially evolving Stratford ramp flow is investigated by numerical simulations based on the two--dimensional incompressible Navier-Stokes equations. The simulations have shown that beyond certain Reynolds numbers, instability waves are developing even when no "controlled " disturbances are introduced. These instability waves increase the momentum exchange between the outer and inner part of the boundary layer and thus can suppress the massive separation which would have occurred for the steady laminar flow under the same adverse pressure gradient. This natural instability can be exploited by introducing controlled disturbances (in the present case, by periodic blowing and suction through a slot). For example, a small separation bubble, which occurred at the upstream end of the Stratford ramp when no controlled disturbances were introduced, could be completely suppressed by periodically forcing the flow with the frequency that was observed for the "natural " (uncontrolled) case. However, for this "controlled " case another separation bubble may be generated further downstream. By carefully adjusting the forcing frequency (to about half of the natural frequency), the size and intensity of the newly generated separation bubble can be greatly reduced. When the Reynolds number was increased, extensive separation occurred without forcing, although instability waves were developing as for the low Reynold number case. However, the separation could again be suppressed by periodic forcing with large amplitudes. Furthermore, the required forcing

Citations

58 Boundary layer theory – Schlichting - 1968
8 Oscillatory Blowing: A Tool to Delay Boundary-Layer Separation – Seifert, Bachar, et al. - 1993
6 Active Control of LaminarTurbulent Transition – Liepmann, Nosenchuck - 1982
6 Control of turbulence – Lumley, Blossey - 1998
6 An experimental flow with zero skin friction throughout its region of pressure rise – Stratford - 1956
5 Active Control of Instabilities in Laminar Boundary-Layer Flow. Part I. An Overview," (submitted – Joslin, Erlebacher, et al. - 1994
5 Tollmien-Schlichting Wave Cancellation – Milling - 1981
4 A compactdifference scheme for the Navier-Stokes equations in vorticity-velocity formulation – Meitz, Fasel - 1999
4 The unsteady structure of two--dimensional steady laminar separation – Ripley, Pauley - 1993
3 An experimental and theoretical study of a boundary layer approaching separation. AIAA Paper 97--0867 – Elsberry, Likhachev, et al. - 1997
3 The structure and behavior of laminar separation bubbles – Gaster - 1967
3 Outflow boundary conditions for spatial Navier-Stokes simulations of transitional boundary layers – Kloker, Konzelmann, et al. - 1993
2 Control of flow separation: energy conservation, operational efficiency, and safety – Chang - 1976
2 Micro--Electro-- Mechanical--Systems (MEMS) and fluid flows – Ho, Tai - 1998
2 K.: Design Tradeoffs on Scramjet Engine Integrated Hypersonic Waverider Vehicles – O'Neill, M - 1993
2 Direct numerical simulation of two-dimensional incompressible laminar flow over Stratford ramp, DFD97 – Zhang, Fasel - 1997
1 Unsteady separation from the leading edge of a thin airfoil – Degani, Li, et al. - 1996
1 Effect of laminar flow control by suction on separation – Masad, Abid - 1996
1 The forced mixing layer between parallel streams – Oster, Wygnanski - 1982
1 Vectoring and small scale motions effected in free shear flows using synthetic jet actuators," AIAA Paper 97--0213 – Smith, Glezer - 1997
1 Control of laminar separation over airfoils by acoustic excitation – Zaman, McKinzie - 1991
1 Spatial Direct Numerical Simulation of Goertler Vortices – Zhang, Fasel - 1997