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https://turbmodels.larc.nasa.gov/onerawingnumerics_val.html

This is a tutorial of a cavity flow for AENG 418 class

AENG344
Problem 9.14 
Consider a diamond-wedge airfoil such as shown in Figure 9.36, with a half-angle 10 degrees. The airfoil is at an angle of attack of 15 degree to a Mach 3 freestream. Calculate the lift and wave-drag coefficients for the airfoil

This tutorial aims to showcase how to set up a compressible analysis. An aircraft wing geometry is used.

Tutorial project for a flow analysis of a pipe junction. The project only provides the geometry to start with. See our tutorials section to have a look at the step-by-step instructions to set up the simulation.

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