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  • 學位論文

二維方柱橫向與扭轉向振動耦合之氣動力研究

Aerodynamic forces of a square prism in transverse and torsional coupled motion

指導教授 : 盧博堅

摘要


本研究將探討一二維方柱體在受強制振動影響下,改變其橫風向與扭轉向振動間的頻率比及二維方柱之偏心量,進而瞭解橫風向與扭轉向振動間發生耦合時,結構物所產生之氣動力現象。 結果顯示,當Fr大於1.0時,在勁度中心往上游偏離,偏心量為10%時可得最小的擾動昇力係數峰值及渦散頻率的尾跡風速;而在勁度中心往上游偏離,偏心量為20%可得最大的擾動昇力係數峰值及渦散頻率的尾跡風速。當Fr等於1.0時,在勁度中心往上游偏離,偏心量為10%時可得最大的擾動昇力係數峰值及渦散頻率的尾跡風速;而在勁度中心往上游偏離,偏心量為20%可得最小的擾動昇力係數峰值及渦散頻率的尾跡風速。與Fr大於1.0正好相反。當Fr小於1.0時,在勁度中心無偏離時,可得最大的擾動昇力係數峰值及渦散頻率的尾跡風速;而最小值則不一定發生在哪一個偏心上。

並列摘要


Wind tunnel measurements were performed to study the aerodynamic phenomenon of a two dimensional prism when the mass center separates from the center in transverse and torsional coupled vibration modes. When the torsion/transverse frequency ratio (Fr) is greater than 1.0, as long as the eccentricity is introduced in the upstream direction at 10%, the spectral peaks of the lift fluctuation coefficient and the vortex shedding reach a minimum value compared with other eccentricities. However, as the eccentricity increases to 20%, the spectral peaks reach a maximum value. Whereas when Fr=1, eccentricity 10% and 20% in the upstream direction, the spectral peaks of lift fluctuation coefficient and vortex shedding show the opposite trend. A maximum value is obtained when Fr is smaller than 1.0 and without eccentricity. However, there is no obvious trend for the minimum value.

參考文獻


1. Bearman‚ P.W. and Luo‚ S.C.‚"Investigation of the aerodynamic instability of a square-section cylinder by force oscillation".J.Fluid Struc.2‚161-176.(1988)
2. Bearman‚ P.W. and Obasaju‚ E.D.‚"An experimental study of pressure fluctuation on fixed and oscillating square-
3. Bearman‚ P.W. and Graham‚J.M.R.‚"Vortex shedding from bluff bodies in oscillatory flow"‚:A report on Euromech 119. J.
Fluid Mech.99‚225-245.(1980)
4. Bearman‚ P.W.‚" Vortex shedding from oscillating bluff bodies".Ann‚Rev.Fluid Mech.16‚195-222.(1984)

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