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Dynamics and Stability of Spinning Membranes

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Figure

Figure 1.3: Solar array wing on the International Space Station (NASA, 2006).
Figure 2.1: Mechanical test setup.
Figure 2.5: Experimentally derived wave numbers for Ka-20 test sample, at ω = 855, 793 , and 783 rpm.h=50 µm corresponds to the membrane thickness.
Figure 2.6.ω
+7

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Outline

Comparison of Present Theory with Membrane Theory, Nonlinear Simulations, and Experiments Nonlinear Behavior Potential Application Test Case: Linear Spinning Clamped Plate

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