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Post by Br. Marius on Mar 31, 2015 13:29:25 GMT
For a uniform blade, the viscous damping ratio and rotating natural frequency of torsion mode in vacuum chamber were determined to be 1% and 4/rev. If the rotor speed is doubled, calculate the new rotating natural frequency and damping ratio.
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Post by Br. Marius on Apr 1, 2015 19:02:01 GMT
\(\nu_{\theta2}=2.18/rev\) \(\zeta_2=0.9%\) Work is attached. Attachments:HW7-3.docx (20.25 KB)
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Deleted
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Post by Deleted on Apr 1, 2015 22:18:28 GMT
Yep, same here.
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