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Showing 1 to 1 of 1 for “"Optimum aerodynamic design"”.
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Gradient-Based Optimum Aerodynamic Design Using Adjoint Methods
… are applied to a pressure-matching inverse design problem of quasi 1-D nozzle flows. Pontryagin’s Minimum Principle is used to derive the adjoint system and the reduced gradient of the cost functional. The properties of adjoint variables at the sonic throat and the shock location are …