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Advances in Acoustics and Vibration
Table of Contents
Special Issues
Advances in Acoustics and Vibration
/
2016
/
Article
/
Fig 2
/
Research Article
Stability Analysis of a Flutter Panel with Axial Excitations
Figure 2
N.D. natural frequency variations with respect to dynamic pressure ratio: Ma = 2,
, and
= 2.47 Ć 10
ā6
.