Validation studies were performed on the aerodynamic, aerothermal, and aerothermoelastic configurations of the solver, which were then used to investigate the aforementioned subjects. To facilitate this examination, an aerothermoelastic solver was created by coupling solvers for the structural elasticity and thermal diffusion equations to a Reynolds averaged Navier-Stokes (RANS) solver. This dissertation examines the following subjects important to hypersonic aerothermoelastic flows: aerodynamic heating on a double-wedge airfoil, active cooling on a double-wedge airfoil, and aerothermoelastic panel utter with deformable supports.
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