Inviscid compressible flow past multi-element aerofoils

2 volsSIGLEAvailable from British Library Document Supply Centre- DSC:D67423/86 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Simulation of inviscid blade row interaction using a linear and a non-linear method

Available from British Library Document Supply Centre- DSC:8019.3153(RR-PNR--90886) / BLDSC - British Library Document Supply CentreSIGLEGBUnited Kingdo

Simulation of inviscid blade row interaction using a linear and a non-linear method

Available from British Library Document Supply Centre- DSC:8019.3153(RR-PNR--90886) / BLDSC - British Library Document Supply CentreSIGLEGBUnited Kingdo

Aerodynamic Design Optimization on Unstructured Meshes Using the Navier-Stokes Equations

A discrete adjoint method is developed and demonstrated for aerodynamic design optimization on unstructured grids. The governing equations are the three-dimensional Reynolds-averaged Navier-Stokes equations coupled with a one-equation turbulence model. A discussion of the numerical implementation of the flow and adjoint equations is presented. Both compressible and incompressible solvers are differentiated and the accuracy of the sensitivity derivatives is verified by comparing with gradients obtained using finite differences. Several simplifying approximations to the complete linearization of the residual are also presented, and the resulting accuracy of the derivatives is examined. Demonstration optimizations for both compressible and incompressible flows are given. * Graduate Student, Aerospace and Ocean Engineering Department, Student Member AIAA. + Senior Research Scientist, Aerodynamic and Acoustic Methods Branch, Fluid Mechanics and Acoustics Division, Assoc. Fellow, AIAA. Co..