Accelerating Computational Fluid Dynamics Based Aeroelastic Predictions Using System Identification
Author:
Affiliation:
1. Oklahoma State University, Stillwater, Oklahoma 74078
2. NASA Dryden Flight Research Center, Edwards, California 93523
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2737
Reference10 articles.
1. Reduced order models in unsteady aerodynamics
2. 4Ljung, L., System Identifi cation: Theory for the User, Prentice-Hall, Upper SaddleRiver, NJ,1987, pp.1, 2.
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