By Henry M. Paynter
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Extra resources for Analysis and design engineering systems
FB 81–33. DFVLR. , Liu, C. F. & Shyu, J. Y. 1990 Control of wall-separated ﬂow by internal acoustic excitation. AIAA J. 28, 1440–1446. -H. Fernholz and F. Urzynicok  Huang, L. , Bryant, T. D. & Maestrello, L. 1988 The eﬀect of acoustic forcing on trailing edge separation and near wake development of an airfoil. AIAA Paper 88–3531-CP.  Huang, L. , Maestrello, L. & Bryant, T. D. 1987 Separation control over an airfoil at high angles of attack by sound emanating from the surface. AIAA Paper 87–1261 .
Each curve has a saturation value Ecohmax at a diﬀerent height and at a diﬀerent streamwise location x/h. This behavior is typical of a Kelvin-Helmholtz instability. A comparison of Fig. 84) occurs at f = 120 Hz which is not the curve with the absolute maximum (f = 51 Hz) but the curve with the highest values of Ecoh very close to the fence, since here the ﬂow manipulation is most eﬀective in reducing the reattachment length. For this case and single frequency excitation, PIV measurements were made which show the expected roll-up of the shear layer to a large coherent structure just downstream of the fence without vortex pairing (not shown here, but see ).
2001 The manipulated transitional backward-facing step ﬂow: an experimental and direct numerical simulation investigation. Eur. J. Mech. B/Fluids 20, 25–46. -H. Fernholz and F. Urzynicok  Werlé, H. 1960 Essais de souﬄage au tunnel hydrodynamique a visualisation. Note Technique 61. ONERA.  Williams, D. , Bernhardt, J. -M. 1991 The mechanism of ﬂow control on a cylinder with the unsteady bleed technique. AIAA Paper 91–0039 .  Wu, J. M. & Wu, J. Z. 1992 Vortex lift at a very high angle of attack with massively separated unsteady ﬂow.