Flutter Analysis with Stabilized Finite Elements based on the Linearized Frequency-domain Approach
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Reference36 articles.
1. Uncertainty Quantification in Aeroelasticity
2. Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration
3. Active Flutter Control using an Adjoint Method
4. Adjoint-Based Sensitivity Formulation for Fully Coupled Unsteady Aeroelasticity Problems
5. CFD-based Aeroelastic Adjoint Sensitivities for Flight Vehicle Weight Minimization Using Sizing and Shape Design Variables
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