An Experimental investigation of means to suppress the flutter motion of elastically suspended cylinders exposed to uniform cross flow

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040 ⊔ ⊔ ‡aTRAAL ‡beng ‡erda ‡cTRAAL
049 ⊔ ⊔ ‡aMAIN
086 0 ⊔ ‡aD 217.22: 72-6
100 1 ⊔ ‡aBerezow, J., ‡eauthor.
245 1 3 ‡aAn Experimental investigation of means to suppress the flutter motion of elastically suspended cylinders exposed to uniform cross flow / ‡cby J. Berezo, D. W. Sallet.
264 ⊔ 1 ‡aWhite Oak, Maryland : ‡bUnited States Naval Ordance Laboratory, ‡c1972.
300 ⊔ ⊔ ‡a1 volume (various pagings) : ‡billustrations, figures, tables ; ‡c28 cm.
336 ⊔ ⊔ ‡atext ‡btxt ‡2rdacontent
337 ⊔ ⊔ ‡aunmediated ‡bn ‡2rdamedia
338 ⊔ ⊔ ‡avolume ‡bnc ‡2rdacarrier
490 0 ⊔ ‡aNOLTR (Series) ; ‡v72-6
500 ⊔ ⊔ ‡a"Project No. ORD-35B-501/UR12-301-001."
500 ⊔ ⊔ ‡a"28 February 1972."
504 ⊔ ⊔ ‡aIncludes bibliographical references (page 33).
520 ⊔ ⊔ ‡aWhen 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.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aFlutter (Aerodynamics).
650 ⊔ 0 ‡aVortex shedding.
710 2 ⊔ ‡aNaval Ordnance Laboratory (White Oak, Md.). ‡eissuing body.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
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