Wing Design via Numerical Optimization: Are we there yet?

24 April 2014
4:00 pm to 5:00 pm
Wing Design via Numerical Optimization: Are we there yet?
Prof. Joaquim Martins
University of Michigan

[1] G. K. W. Kenway, G. J. Kennedy, and J. R. R. A. Martins. Scalable parallel approach for high-fidelity steady-state aeroelastic analysis and derivative computations. AIAA Journal, 2014. (In press).
[2] G. K. W. Kenway and J. R. R. A. Martins. Multi-point high-fidelity aerostructural optimization of a transport aircraft configuration. Journal of Aircraft, 51(1):144–160, 2014.
[3] Z. Lyu and J. R. R. A. Martins. Aerodynamic design optimization studies of a blended-wing-body aircraft. Journal of Aircraft, 2014. (In press).
[4] R. P. Liem, G. K. Kenway, and J. R. R. A. Martins. Multi-point, multi-mission, high-fidelity aerostructural optimization of a long-range aircraft configuration. In Proceedings of the 14th AIAA/ISSMO Mul- tidisciplinary Analysis and Optimization Conference, Indianapolis, IN, Sept. 2012.