Multi-objective aerodynamic shape optimization for unsteady viscous flows

Author:

Nadarajah Siva K.,Tatossian Charles

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Control and Optimization,Mechanical Engineering,Aerospace Engineering,Civil and Structural Engineering,Software

Reference33 articles.

1. Adamczyk JJ (1984) Model equation for simulating flows in multistage turbomachinery. NASA Technical Memorandum 86869, November 1984. Technical report

2. Anderson WK, Venkatakrishnan V (1999) Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation. Comput Fluids 28(4–5):443–480

3. Bennet RM, Walker CE (1999) Computational test cases for a rectangular supercritical wing undergoing pitching oscillations. Technical report, NASA/TM-1999-209130, NASA Langley Research Center, Hampton, VA, April 1999

4. Duta MC, Giles MB, Campobasso MS (2002) The harmonic adjoint approach to unsteady turbomachinery design. Int J Numer Methods Fluids 40:323–332

5. Elliot J, Peraire J (1996) Aerodynamic design using unstructured meshes. AIAA Paper 96-1941

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