Wake flow in adverse pressure gradient

Abstract In the interest of improving the predictability of high-lift systems at maximum lift conditions, a series of fundamental experiments were conducted to study the effects of adverse pressure gradient on a wake flow. Mean and fluctuating velocities were measured with a two-component laser-Doppler velocimeter. Data were obtained for several cases of adverse pressure gradient, producing flows ranging from no reversed flow to massively reversed flow. While the turbulent Reynolds stresses increase with increasing size of the reversed flow region, the gradient of Reynolds stress (− ∂ uv / ∂ y) does not. Computations using various turbulence models were unable to reproduce the reversed flow.

[1]  Desmond Adair,et al.  Characteristics of merging shear layers and turbulent wakes of a multi-element airfoil , 1988 .

[2]  R. Nelson,et al.  An experimental investigation of wake development in arbitrary pressure gradients , 1999 .

[3]  G. Brune,et al.  Experimental investigation of the confluent boundary layer of a multielement low speed airfoil , 1983 .

[4]  Steven P. Schneider,et al.  Wake measurements in a strong adverse pressure gradient , 1994 .

[5]  Stuart E. Rogers Progress in high-lift aerodynamic calculations , 1993 .

[6]  Robert J. Mcghee,et al.  Flowfield measurements about a multi-element airfoil at high Reynolds numbers , 1993 .

[7]  P. Spalart A One-Equation Turbulence Model for Aerodynamic Flows , 1992 .

[8]  Stuart E. Rogers,et al.  An upwind differencing scheme for the incompressible Navier-Stokes equations , 1991 .

[9]  Franz Durst,et al.  Turbulent Shear Flows I , 1979 .

[10]  P. Pot A wake boundary layer mixing experiment , 1979 .

[11]  Frederick Roos Experimental studies of wake retardation in a simulated high-lift-system flow field , 1997 .

[12]  Stuart E. Rogers,et al.  Upwind differencing scheme for the time-accurate incompressible Navier-Stokes equations , 1990 .

[13]  F. Menter ZONAL TWO EQUATION k-w TURBULENCE MODELS FOR AERODYNAMIC FLOWS , 1993 .

[14]  F. Menter Improved two-equation k-omega turbulence models for aerodynamic flows , 1992 .

[15]  R. Henkes,et al.  Experimental investigation of an adverse pressure gradient wake and comparison with calculations , 1997 .