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Sensitivity calculations for a 2D, inviscid, supersonic forebody problemThe 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.
Document ID
19930017815
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Borggaard, Jeff
(Virginia Polytechnic Inst. Blacksburg., United States)
Burns, John A.
(Virginia Polytechnic Inst. Blacksburg., United States)
Cliff, Eugene
(Virginia Polytechnic Inst. Blacksburg., United States)
Gunzburger, Max
(Virginia Polytechnic Inst. Blacksburg., United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
ICASE-93-13
AD-A265066
NASA-CR-191444
NAS 1.26:191444
Report Number: ICASE-93-13
Report Number: AD-A265066
Report Number: NASA-CR-191444
Report Number: NAS 1.26:191444
Accession Number
93N27004
Funding Number(s)
CONTRACT_GRANT: F49620-92-J-0078
CONTRACT_GRANT: NAS1-19480
CONTRACT_GRANT: NSF INT-89-22490
CONTRACT_GRANT: AF-AFOSR-0179-90
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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