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Advances in Acoustics and Vibration
Table of Contents
Special Issues
Advances in Acoustics and Vibration
/
2016
/
Article
/
Fig 3
/
Research Article
Stability Analysis of a Flutter Panel with Axial Excitations
Figure 3
Stability plot for the flutter panel with respect to axial excitation frequency and dynamic pressure ratio: Ma = 2,
,
= 2.47 × 10
−6
,
= 4.39 × 10
−5
, and
.