Side-Wall Effects on the Global Stability of Swept and Unswept Supercritical Wings at Buffet Conditions

2022 ◽  
Author(s):  
Andrea Sansica ◽  
Atsushi Hashimoto ◽  
Shunsuke Koike ◽  
Toshinori Kouchi
2021 ◽  
Vol 239 ◽  
pp. 109797
Author(s):  
Chaobang Yao ◽  
Jianghao Huang ◽  
Xiaoshuai Sun ◽  
Jiawei Yu ◽  
Dakui Feng

1995 ◽  
Vol 117 (1) ◽  
pp. 17-23 ◽  
Author(s):  
G. Papadopoulos ◽  
M. V. O¨tu¨gen

The incompressible turbulent flow over a backward-facing step in a rectangular duct was investigated experimentally. The side wall effects on the core flow were determined by varying the aspect ratio (defined as the step span-to-height ratio) from 1 to 28. The Reynolds number, based on the step height and the oncoming free-stream velocity, was 26,500. Detailed velocity measurements were made, including the turbulent stresses, in a region which extended past the flow reattachment zone. Wall static pressure was also measured on both the step and flat walls. In addition, surface visualizations were obtained on all four walls surrounding the separated flow to supplement near-wall velocity measurements. The results show that the aspect ratio has an influence on both the velocity and wall pressure even for relatively large aspect ratios. For example, in the redevelopment region downstream of reattachment, the recovery pressure decreases with smaller aspect ratios. The three-dimensional side wall effects tend to slow down the relaxation downstream of reattachment for smaller aspect ratios as evidenced by the evolution of the velocity field. For the two smallest aspect ratios investigated, higher centerplane streamwise and transverse velocities were obtained which indicate a three-dimensional mean flow structure along the full span of the duct.


1999 ◽  
Vol 103 (1021) ◽  
pp. 139-142 ◽  
Author(s):  
L. W. Traub

AbstractAn incompressible method is presented to predict the upwash corrections associated with vortical flow as a result of wind-tunnel side wall effects. An image system is used to simulate the tunnel side walls which are assumed to be solid. An integral expression is formulated, representing the average upwash induced over the wing by the image system. Wall effects may be determined for flows with and without vortex breakdown. Comparisons of the results with upwash predictions from a Navier-Stokes study show close accord. The upwash expression also displayed the ability to successfully predict corrections for flows involving vortex breakdown.


2009 ◽  
Vol 11 (5) ◽  
pp. 053016 ◽  
Author(s):  
C Gollwitzer ◽  
A N Spyropoulos ◽  
A G Papathanasiou ◽  
A G Boudouvis ◽  
R Richter

2001 ◽  
Vol 24 (3) ◽  
pp. 405-408 ◽  
Author(s):  
P.-E. Roche ◽  
B. Castaing ◽  
B. Chabaud ◽  
B. Hébral ◽  
J. Sommeria

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