Studies of the continuous and discrete adjoint approaches to viscous automatic aerodynamic shape optimization
- 11 June 2001
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 18 references indexed in Scilit:
- Optimum Aerodynamic Design Using the Navier-Stokes EquationsTheoretical and Computational Fluid Dynamics, 1998
- Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Optimum aerodynamic design using the Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Optimum aerodynamic design using CFD and control theoryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Aerodynamic shape optimization of wing and wing-body configurations using control theoryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Aerodynamic design via control theoryJournal of Scientific Computing, 1988
- Optimal Shape Design for Elliptic SystemsPublished by Springer Science and Business Media LLC ,1984
- Wing Design by Numerical OptimizationJournal of Aircraft, 1978
- NUMERICAL DESIGN OF TRANSONIC AIRFOILS**The work presented in this paper is supported by the AEC Computing and Applied Mathematics Center, Courant Institute of Mathematical Sciences, New York University, under Contract AT(30-1)-1480 with the U. S. Atomic Energy Commission.Published by Elsevier BV ,1971
- Optimal Control of Systems Governed by Partial Differential EquationsPublished by Springer Science and Business Media LLC ,1971