Flutter Analysis of Aerostructures Test Wing with Test Validated Structural Dynamic Model
Author:
Affiliation:
1. NASA Dryden Flight Research Center, Edwards, California 93523-0273
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031257
Reference19 articles.
1. Finite Element Model Updating in Structural Dynamics
2. Finite Element Model Tuning Using Measured Mass Properties and Ground Vibration Test Data
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