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Mathematical Problems in Engineering
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Mathematical Problems in Engineering
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2017
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Article
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Fig 2
/
Research Article
New Look at Nonlinear Aerodynamics in Analysis of Hypersonic Panel Flutter
Figure 2
Positive LCO deflection peak versus dynamic pressure for a square panel at Ma = 5, 10, and
at different temperatures: (a)
; (b)
.
(a)
(b)