Ground Vibration Test Identified Structure Model for Flutter Envelope Prediction
Author:
Affiliation:
1. ZONA Technology
2. Arizona State University
3. NASA Dryden Flight Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4856
Reference5 articles.
1. Unsteady supersonic computations of arbitrary wing-body configurations including external stores
2. 3Cole,S.R."FlutterofaLow-Aspect-RatioRectangularWing,"NASATechnicalMemorandum4116,1989.
3. 4Ljung,L.SystemIdentification-TheoryfortheUser.PrenticeHall,UpperSaddleRiver,NJ,1999.
4. Subspace Identification for Linear Systems
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