NASA NTRS · 19940004672
A comparison of optimization-based approaches for solving the aerodynamic design problem
Abstract
Three optimization-based methods for solving aerodynamic design problems are compared. The Euler equations for one-dimensional duct flow was used as a model problem, and the three methods are compared for efficiency, robustness, and implementation difficulty. The smoothness of the design problem with respect to different shock-capturing finite difference schemes, and in the presence of grid refinement, is investigated.
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Frank, Paul D., Shubin, Gregory R.. 1990-01-01. A comparison of optimization-based approaches for solving the aerodynamic design problem. https://ntrs.nasa.gov/citations/19940004672
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