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Theaimofthisworkistoinvestigatenumericallythermalbarriercoating (TBC) systems applied to realistic rocket thrust chamber conditions. A global full parametric three-dimensional (3D) modeling approach for cooled rocket thrust chambers is presented to be able to simulate the §uidstructure interaction (FSI) phenomena involved. In a subsequent analysis step, realistic mechanical and thermal boundary conditions are extractedfromcriticaldesignregionsoftheglobalmodelandappliedtoa local¦niteelementmodel(FEM)toanalyzepossibleTBCdelaminations by means of a Fracture Mechanics (FM) approach.

progress in propulsion physics

Fluid-structure interaction analysis applied to thermal barrier coated cooled rocket thrust chambers with subsequent local investigation of delamination phenomena