Search
CSV
RISConstrained Adjoint Based Aerodynamic Shape Optimization of a Single Stage Transonic Compressor
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper develops a discrete adjoint formulation for the constrained aerodynamic shape optimization in a multistage turbomachinery environment. The adjoint approach for viscous internal flow problems and the corresponding ...
Optimum Shape Design for Multirow Turbomachinery Configurations Using a Discrete Adjoint Approach and an Efficient Radial Basis Function Deformation Scheme for Complex Multiblock Grids
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper proposes a framework for fully automatic gradientbased constrained aerodynamic shape optimization in a multirow turbomachinery environment. The concept of adjointbased gradient calculation is discussed and the ...