作者: Oktay Baysal , Kaveh Ghayour
DOI: 10.2514/2.1269
关键词:
摘要: A continuous adjoint approach is developed to obtain the sensitivity derivatives for Euler equations. The completederivationofthecostateequations andtheirtransversality (boundary)conditionsarepresented. Both state and costate equations are second-order e nite volume discretized unstructured meshes, they coupled with a constrained optimization algorithm. Also integrated into overall methodology geometry parameterization method shape optimization, dynamic mesh evolution consequent adaptations. For proof of concept, three transonic airfoil problems presented. This accepts general cost functionals, which not necessarily functions pressure only. It also shown that switch natural coordinate system in conjunction reduction governing equation control surface results integrals only function tangential derivativesof variables. Thisapproach eliminates need fornormal derivativecomputations can be erroneous.