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Advances in Acoustics and Vibration
Table of Contents
Special Issues
Advances in Acoustics and Vibration
/
2016
/
Article
/
Fig 5
/
Research Article
Stability Analysis of a Flutter Panel with Axial Excitations
Figure 5
Stability plot for the flutter panel with respect to air/panel density ratio and dynamic pressure ratio: Ma = 2,
,
= 2.47 Ć 10
ā6
, and
.