======Plane Wake Near a Swept Wing====== =====Experiments by Pailhas and Jayaraman===== ---- ====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//. ---- Indexed data: case : 040 title : Plane Wake Near a Swept Wing author* : Pailhas, Jayaraman year : 1989 type : EXP flow_tag* : 3d, wake, streamlined_body