Aerodynamic Parameter Adaptation of CFD-Based Reduced-Order Models
Author:
Affiliation:
1. Stanford University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-328
Reference37 articles.
1. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.
2. Reduced-order fluid/structure modeling of a complete aircraft configuration
3. Reduced order unsteady aerodynamic and aeroelastic models using Karhunen-Loeve eigenmodes
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1. Stable and Efficient Galerkin Reduced Order Models for Non-Linear Fluid Flow;6th AIAA Theoretical Fluid Mechanics Conference;2011-06-14
2. Calculation of Unsteady Control Surface Aerodynamics using Reduced-Order Models;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
3. Stable Galerkin reduced order models for linearized compressible flow;Journal of Computational Physics;2009-04
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