Introduction
This tutorial illustrates the setup and simulation of store separation from an airplane wing.The
flow is inviscid and compressible. The objective of this simulation is to model the motion of the store using the Six Degrees of Freedom (6DOF) solver in FLUENT. The results of the FLUENT simulation are compared with the results computed from a series of wind tunnel tests. For the details about the wind tunnel testing, refer to Appendix. This tutorial demonstrates how to do the following

  Use the DEFINE SDOF PROPERTIES macro to specify the mass matrix and any external forces/moments

 Use the dynamic mesh (DM) feature in FLUENT

Set up a compressible, transonic flow (Mach 1.2) in FLUENT

Set the boundary conditions

 Set up dynamic adaption

 Obtain a first order solution using the density-based implicit solver