How to do this step in CFD, Ansys Fluent for a Supersonic Flow Over a Wedge of 10 Degree angle.
( Plot the height above the wall (y) vs velocity (u direction) from the wall to the freestream (velocity profile) of the airfoil or the high-speed geometry. Three locations should be provided towards the leading edge of the geometry, roughly the middle, and towards the end.)
I assumed you have made the geometry & done with the meshing part. If you didn't these 2 are easy part. Just Go to Space clan & draw the dimensions of air foil you need. Then go to meshing paet & make simple grid( for beginers).NNowcomes the setup part. In this part choose a model ( you can take laminar) & set boundry conditon which is known to you.Then ggo to Run section & run it for steady condition.Now rrun part has completed. Now go solution part. Click on graphic part. Select steamlines from feom it & draw it on wall.Then pplot absolute velocity.Now ssave it you have your contours.
How to do this step in CFD, Ansys Fluent for a Supersonic Flow Over a Wedge of 10 Degree angle. ( Plot the height above the wall (y) vs velocity (u direction) from the wall to the freestream (velocity...