Numerical Results - Lesson 7

In this lesson, you will learn how to:

  1. Look at the lift and drag forces on the wing
  2. Look at the lift and drag coefficients on the wing
  3. Create pressure and Mach contours
  4. Look at the Boundary Layer before and after the shock
  5. Create velocity vectors at the trailing edge plane
  6. View trailing vortices
  7. Plot Pressure Coefficient at spanwise fraction .2
  8. Compare Fluent Pressure Coefficient to experimental data