An Experimental investigation of means to suppress the flutter motion of elastically suspended cylinders exposed to uniform cross flow /
by J. Berezo, D. W. Sallet.
Description
- Language(s)
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English
- Published
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White Oak, Maryland : United States Naval Ordance Laboratory, 1972.
- Summary
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When an elastically supported circular cylinder is brought into steady fluid flow, flutter motions occur when it is subjected to flow velocities which exceed a certain critical velocity. The flow-induced vibrations can be reduced by modifying the surface of the cylinder. This report discusses the effects of 21 surface modifications on the flow-induced vibrations. It is seen that surface modifications can reduce the amplitudes of the flutter motions.
- Note
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"Project No. ORD-35B-501/UR12-301-001."
"28 February 1972."
- Physical Description
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1 volume (various pagings) :
illustrations, figures, tables ;
28 cm.
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