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Aerodynamic design and optimization in one shotThis paper describes an efficient numerical approach for the design and optimization of aerodynamic bodies. As in classical optimal control methods, the present approach introduces a cost function and a costate variable (Lagrange multiplier) in order to achieve a minimum. High efficiency is achieved by using a multigrid technique to solve for all the unknowns simultaneously, but restricting work on a design variable only to grids on which their changes produce nonsmooth perturbations. Thus, the effort required to evaluate design variables that have nonlocal effects on the solution is confined to the coarse grids. However, if a variable has a nonsmooth local effect on the solution in some neighborhood, it is relaxed in that neighborhood on finer grids. The cost of solving the optimal control problem is shown to be approximately two to three times the cost of the equivalent analysis problem. Examples are presented to illustrate the application of the method to aerodynamic design and constraint optimization.
Document ID
19920039523
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ta'asan, Shlomo
(Weizmann Institute of Science, Rehovot, Israel; ICASE, Hampton VA, United States)
Kuruvila, G.
(Vigyan, Inc. Hampton, VA, United States)
Salas, M. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 92-0025
Accession Number
92A22147
Distribution Limits
Public
Copyright
Other

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