Aeroelastic Analysis of F-16 and F-18/A Configurations Using Adapted CFD-Based Reduced-Order Models
Author:
Affiliation:
1. Stanford University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-2364
Reference36 articles.
1. Calculation of Wing Flutter by a Coupled Fluid-Structure Method
2. Aeroelastic Dynamic Analysis of a Full F-16 Configuration for Various Flight Conditions
3. Application of a three-field nonlinear fluid–structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter
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