Plotting Contour of Velocity Magnitude Results > Graphics and Animations > Contours > Set Up… Change the parameters as per below and click Display. Save the picture the same way as you did for Residual History but in this case, name it Lab 2 “CFD Zoom in where you can see the airfoil clearly and the change in contour Contour of Velocity Magnitude”. levels around the airfoil. Plotting Velocity Vectors at Trailing Edge Results > Graphics and Animations > Vectors > Set Up… Change parameters as per below and click Display. Save the picture the same way as you did for Residual History but in this case, name it Lab 2 “CFD Zoom in on the trailing edge. Vectors of Velocity at Trailing Edge”. Plotting Streamlines Close to Airfoil Surface Results > Graphics and Animations > Contours > Set Up… Change parameters as per and click Display. Save the picture the same way as you did for Residual History but in this case, name it Lab 2 “CFD Adjust Min and Max values until streamlines cover the airfoil. Streamlines Close to Surface”.
Plotting Contour of Velocity Magnitude Results > Graphics and Animations > Contours > Set Up… Change the parameters as per below and click Display. Save the picture the same way as you did for Residual History but in this case, name it “CFD Lab 2 Contour of Velocity Magnitude”. Zoom in where you can see the airfoil clearly and the change in contour levels around the airfoil. Plotting Velocity Vectors at Trailing Edge Results > Graphics and Animations > Vectors > Set Up… Change parameters as per below and click Display. Save the picture the same way as you did for Residual History but in this case, name it “CFD Lab 2 Vectors of Velocity at Trailing Edge”. Zoom in on the trailing edge. Plotting Streamlines Close to Airfoil Surface Results > Graphics and Animations > Contours > Set Up… Change parameters as per and click Display. Save the picture the same way as you did for Residual History but in this case, name it “CFD Lab 2 Streamlines Close to Surface”. Adjust Min and Max values until streamlines cover the airfoil.