0
TECHNICAL PAPERS

Analysis of Nonlinear Aeroelastic Panel Response Using Proper Orthogonal Decomposition

[+] Author and Article Information
Sean A. Mortara, Joseph Slater

Dept. of Mech. & Mat. Engr., Wright State University, Dayton, Ohio 45435 (937)-775-5085

Philip Beran

Air Force Research Laboratory, VASD, Wright-Patterson AFB, Dayton, Ohio 45433e-mail: philip.beran@wpafb.af.mil

J. Vib. Acoust 126(3), 416-421 (Jul 30, 2004) (6 pages) doi:10.1115/1.1687389 History: Received September 01, 2001; Revised July 01, 2003; Online July 30, 2004
Copyright © 2004 by ASME
Your Session has timed out. Please sign back in to continue.

References

Figures

Grahic Jump Location
1-D panel subject to high speed flow
Grahic Jump Location
First 4 dominant modes of an aeroelastic panel
Grahic Jump Location
Full-Order time deflection showing captured training period (ξ=0.75)
Grahic Jump Location
Comparison of 2, 3, and 4 mode ROM
Grahic Jump Location
LCO amplitude comparison of 3 and 4 Mode ROM
Grahic Jump Location
Limit cycle study with different μ/M
Grahic Jump Location
Stability boundary for varying in-plane loads

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In