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Sensitivity of Lumped Constraints Using the Adjoint MethodAdjoint sensitivity calculation of stress, buckling and displacement constraints may be much less expensive than direct sensitivity calculation when the number of load cases is large. Adjoint stress and displacement sensitivities are available in the literature. Expressions for local buckling sensitivity of isotropic plate elements are derived in this study. Computational efficiency of the adjoint method is sensitive to the number of constraints and, therefore, the method benefits from constraint lumping. A continuum version of the Kreisselmeier-Steinhauser (KS) function is chosen to lump constraints. The adjoint and direct methods are compared for three examples: a truss structure, a simple HSCT wing model, and a large HSCT model. These sensitivity derivatives are then used in optimization.
Document ID
20040086820
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Akgun, Mehmet A.
(Middle East Technical Univ. Ankara, Turkey)
Haftka, Raphael T.
(Florida Univ. Gainesville, FL, United States)
Wu, K. Chauncey
(NASA Langley Research Center Hampton, VA, United States)
Walsh, Joanne L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1999
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 99-1314
Report Number: AIAA Paper 99-1314
Meeting Information
Meeting: 40th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Saint Louis, MO
Country: United States
Start Date: April 12, 1999
End Date: April 15, 1999
Sponsors: American Inst. of Aeronautics and Astronautics, American Helicopter Society, Inc., American Society of Civil Engineers, American Society of Mechanical Engineers, American Society for Composites
Funding Number(s)
CONTRACT_GRANT: NCC1-268
Distribution Limits
Public
Copyright
Public Use Permitted.
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