Aerodynamic shape optimization using preconditioned conjugate gradient methods
- 1 November 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 32 (11) , 2145-2152
- https://doi.org/10.2514/3.12271
Abstract
No abstract availableKeywords
This publication has 19 references indexed in Scilit:
- Improving the efficiency of aerodynamic shape optimizationAIAA Journal, 1994
- Airfoil Shape Optimization Using Sensitivity Analysis on Viscous Flow EquationsJournal of Fluids Engineering, 1993
- Automatic differentiation of advanced CFD codes for multidisciplinary designComputing Systems in Engineering, 1992
- Aerodynamic design optimization using sensitivity analysis and computational fluid dynamicsAIAA Journal, 1992
- Aerodynamic Sensitivity Analysis Methods for the Compressible Euler EquationsJournal of Fluids Engineering, 1991
- Sensitivity analysis, approximate analysis, and design optimization for internal and external viscous flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Preconditioned conjugate gradient methods for the compressible Navier-Stokes equationsAIAA Journal, 1991
- Discretized Newton-relaxation solution of high resolution flux-difference split schemesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Determination of aerodynamic sensitivity coefficients based on the transonic small perturbation formulationJournal of Aircraft, 1990
- Structural optimization by methods of feasible directionsComputers & Structures, 1973