Asymptotic and spectral properties of operator-valued functions generated by aircraft wing model
Author:
Funder
NASA
National Science Foundation
Advanced Research Program-02 of Texas
Publisher
Wiley
Subject
General Engineering,General Mathematics
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1002/mma.456/fullpdf
Reference29 articles.
1. Subsonic flutter suppression using self-straining actuators;Balakrishnan;Journal of the Franklin Institute,2001
2. Mathematical analysis of aircraft wing model in subsonic airflow;Shubov;IMA Journal of Applied Mathematics,2001
3. Asymptotic representations for root vectors of nonselfadjoint operators generated by aircraft wing model in subsonic air flow;Shubov;Journal of Mathematical Analysis and Applications,2001
4. Riesz basis property of root vectors of nonselfadjoint operators generated by aircraft wing model in subsonic air flow;Shubov;Mathematical Methods in the Applied Sciences,2000
5. Asymptotics of the aeroelastic modes and basis property of mode shapes for aircraft wing model;Shubov;Journal of the Fraklin Institute,2001
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3. On fluttering modes for aircraft wing model in subsonic air flow;Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences;2014-12-08
4. Transient Dynamics of Stochastic Structural Systems using a Reduced Order Spectral Function Approach;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA;2012-04-23
5. State space representation of flexible structure dynamics in air flow;Journal of the Franklin Institute;2010-02
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