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Advances in Acoustics and Vibration
Table of Contents
Special Issues
Advances in Acoustics and Vibration
/
2016
/
Article
/
Fig 4
/
Research Article
Stability Analysis of a Flutter Panel with Axial Excitations
Figure 4
Stability plot for the flutter panel with respect to axial excitation frequency and air/panel density ratio: Ma = 2,
,
= 2.47 × 10
−6
,
= 1.27 × 10
−6
, and
.