Multidisciplinary Design Optimization of an Aircraft Wing via a Matrix-Free Approach
Author:
Affiliation:
1. University of Toronto
2. Georgia Institute of Technology
3. University of Michigan, Ann Arbor
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2429
Reference30 articles.
1. Scalable Parallel Approach for High-Fidelity Steady-State Aeroelastic Analysis and Adjoint Derivative Computations
2. Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration
3. A note on the derivation of global stress constraints
4. Application of vector performance optimization to a robust control loop design for a fighter aircraft
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3. A Full-Space Method with Matrix Aggregates for Stress-Constrained Structural Optimization;16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2015-06-18
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