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Multidisciplinary Aerodynamic-Structural Shape Optimization Using Deformation (MASSOUD)This paper presents a multidisciplinary shape parameterization approach. The approach consists of two basic concepts: (1) parameterizing the shape perturbations rather than the geometry itself and (2) performing the shape deformation by means of the soft object animation algorithms used in computer graphics. Because the formulation presented in this paper is independent of grid topology, we can treat computational fluid dynamics and finite element grids in the same manner. The proposed approach is simple, compact, and efficient. Also, the analytical sensitivity derivatives are easily computed for use in a gradient-based optimization. This algorithm is suitable for low-fidelity (e.g., linear aerodynamics and equivalent laminate plate structures) and high-fidelity (e.g., nonlinear computational fluid dynamics and detailed finite element modeling) analysis tools. This paper contains the implementation details of parameterizing for planform, twist, dihedral, thickness, camber, and free-form surface. Results are presented for a multidisciplinary application consisting of nonlinear computational fluid dynamics, detailed computational structural mechanics, and a simple performance module.
Document ID
20040086781
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Samareh, Jamshid A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 21, 2013
Publication Date
September 6, 2000
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 2000-4911
Meeting Information
Meeting: AIAA/NASA/USAF/ISSMO Symposium on Multidisciplinary Analysis and Optimization
Location: Long Beach, CA
Country: United States
Start Date: September 6, 2000
End Date: September 8, 2000
Sponsors: American Inst. of Aeronautics and Astronautics, NASA Headquarters, Department of the Air Force, International Society for Structural and Multidisciplinary Optimization
Distribution Limits
Public
Copyright
Public Use Permitted.
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