Flutter Influence Mode Analysis of High Speed Wing Model

Author:

Ling Zhao,Chen Ji,Yinong Yang,Ziqiang Liu

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference14 articles.

1. Aircraft aeroelasticity handbook;Guan,1994

2. John K. Ramsey, NASA aeroelasticity handbook, Volume 2: Design Guides, NASA/TP-2006-212490-VOL2-PART2, Cleveland: NASA Glenn Research Center, November 2006.

3. M. Baker, P. Lenkey, Parametric flutter analysis of the TCA configuration and recommendation for FFM design and scaling, CRAD-9408-TR-3342, Seattle, WA:The Boeing Company, November 21, 1997.

4. Edwards John W., Schuster David M., Spain Charles V., et al. MAVRIC flutter model transonic limit cycle oscillation test,AIAA paper 2001-1291, Seattle, WA: AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference, April 16-19, 2001.

5. Raveh, D.E, Identification of CFD-based unsteady aerodynamic models for aeroelastic analysis, 44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference. Norfolk, VA. 2003.

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