Discrete adjoint approach for modeling unsteady aerodynamic design sensitivities

Journal Article (Academic article)

A discrete adjoint approach is presented for computing steady and unsteady aerodynamic design sensitivities for compressible viscous flows about airfoil configurations. The nominal flow solver method is based on a harmonic balance solution technique, which is capable of modeling both steady and nonlinear periodic unsteady flows. The computer code for the discrete adjoint solver, which is derived from the nominal harmonic balance solver, has been generated with the aid of the advanced automatic differentiation software tool known as TAF (Transformation of Algorithms in FORTRAN).

Duke Authors

Cited Authors

  • Thomas Jeffrey, P; Hall Kenneth, C; Dowell Earl, H

Published Date

  • 2005

Published In

  • Aiaa Journal

Volume / Issue

  • 43 / 9

Start / End Page

  • 1931 - 1936