======Plane Wake Near a Swept Wing======
=====Experiments by Pailhas and Jayaraman=====
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====Description====
Measurements were taken in the wake in the vicinity of a wing-body junction, with a
symmetric airfoil at an angle of incidence of 15o, and sweep angle of 22o.
The Reynolds number based on chord was \(Re_{chord} = 500,000\).
{{ figs:case040:test40.gif |Flow geometry}}
====Measurement Techniques====
Velocities were measured with X-hot-wire probes.
====Available Measurements====
Data available includes mean velocities and Reynolds stresses across \(x\)-\(z\) planes
at a number of \(y\) locations.
[[case040-plots|Sample plots]] of selected quantities are available.
The data can be downloaded as compressed archives from the links below, or as individual files.
* {{cdata:case040:pwsw-allfiles.zip|pwsw-allfiles.zip}}
* {{cdata:case040:pwsw-allfiles.tar.gz|pwsw-allfiles.tar.gz}}
^ Mean Velocity and Reynolds Stress Measurements ^^
| \(y\) location | File |
| \(y=10\) mm | {{cdata:case040:si4fy010.dat|si4fy010.dat}} |
| \(y=20\) mm | {{cdata:case040:si4fy020.dat|si4fy020.dat}} |
| \(y=30\) mm | {{cdata:case040:si4fy030.dat|si4fy030.dat}} |
| \(y=40\) mm | {{cdata:case040:si4fy040.dat|si4fy040.dat}} |
| \(y=50\) mm | {{cdata:case040:si4fy050.dat|si4fy050.dat}} |
| \(y=60\) mm | {{cdata:case040:si4fy060.dat|si4fy060.dat}} |
| \(y=70\) mm | {{cdata:case040:si4fy070.dat|si4fy070.dat}} |
| \(y=80\) mm | {{cdata:case040:si4fy080.dat|si4fy080.dat}} |
| \(y=90\) mm | {{cdata:case040:si4fy090.dat|si4fy090.dat}} |
| \(y=100\) mm | {{cdata:case040:si4fy100.dat|si4fy100.dat}} |
====References====
- Pailhas. G., Jayaraman, V. (1989). Experimental investigation of a three-dimensional wake in the vicinity of a wing-body junction. //DERAT-CERT Report no. 29/5025.20//.
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Indexed data:
case : 040
title : Plane Wake Near a Swept Wing
author* : Pailhas, Jayaraman
year : 1989
type : EXP
flow_tag* : 3d, wake, streamlined_body