Fuel burn Minimization Including Dynamic Aeroelastic Constraint for Free-flying Vehicle Under Geometrically Nonlinear Deformations
Author:
Affiliation:
1. University of Michigan
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-0729
Reference30 articles.
1. A review on non-linear aeroelasticity of high aspect-ratio wings
2. Multidisciplinary aerospace design optimization: survey of recent developments
3. Flutter and post-flutter constraints in aircraft design optimization
4. Scalable Parallel Approach for High-Fidelity Steady-State Aeroelastic Analysis and Adjoint Derivative Computations
5. Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration
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1. A Novel Approach to Trimming Geometrically Nonlinearly Deformed Aircraft for Gradient-Based Optimization Problems;AIAA SCITECH 2024 Forum;2024-01-04
2. Free-Flight Flutter Constraint in Gradient-Based Wing Structural Optimization;AIAA SCITECH 2024 Forum;2024-01-04
3. Development of an Active Wingtip for Aeroelastic Control;Aerospace;2023-08-04
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