Aerodynamic shape optimization of wing and wing-body configurations using control theory
- 9 January 1995
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Aerodynamic optimization studies using a 3-D supersonic Euler code with efficient calculation of sensitivity derivativesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Three-dimensional aerodynamic shape optimization of wings using sensitivity analysisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Aerodynamic shape optimization using preconditioned conjugate gradient methodsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Airfoil Shape Optimization Using Sensitivity Analysis on Viscous Flow EquationsJournal of Fluids Engineering, 1993
- 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
- Aerodynamic design via control theoryJournal of Scientific Computing, 1988
- Solution of the Euler equations for two dimensional transonic flow by a multigrid methodApplied Mathematics and Computation, 1983
- Wing Design by Numerical OptimizationJournal of Aircraft, 1978
- Supercritical Wing Sections IIPublished by Springer Nature ,1975