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NASA NTRS · 19930017815

Sensitivity calculations for a 2D, inviscid, supersonic forebody problem

Abstract

The use of a sensitivity equation method to computer derivatives for optimization based design algorithms are discussed. The problem of designing an optimal forebody simulator is used to motivate the algorithm and to illustrate the basic ideas. Finally, how an existing computational fluid dynamics (CFD) code can be modified to compute sensitivities and a numerical example is presented.

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BibTeXRIS

Borggaard, Jeff, Burns, John A., Cliff, Eugene, Gunzburger, Max. 1993-03-01. Sensitivity calculations for a 2D, inviscid, supersonic forebody problem. https://ntrs.nasa.gov/citations/19930017815

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