Flutter Prediction Using Reduced-Order Modeling with Error Estimation
Author:
Affiliation:
1. University of Toronto, Toronto, Ontario M3H 5T6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061389
Reference63 articles.
1. Multifidelity Optimization of Hybrid Wing–Body Aircraft with Stability and Control Requirements
2. Role of Shocks in the "Sub-Transonic" Flutter Phenomenon
3. Review of unsteady transonic aerodynamics: Theory and applications
4. Non-linear aeroelastic prediction for aircraft applications
5. Computation of Unsteady Transonic Flows by the Indicial Method
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