• Title/Summary/Keyword: 공력 탄성 모형

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Reducing Effect of Wind-induced Vibration on Rectangular Model of Super-Highrise Building with Length of Corners Cutting (초고층 건물의 각주형 단면에 대한 공력 불안정 진동 및 풍진 저감 효과에 관한 실험적 연구)

  • Cheong, Yung-Bea
    • Journal of Korean Society of Steel Construction
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    • v.13 no.3
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    • pp.301-311
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    • 2001
  • For a rectangular-highrise building with aspect ratio about six, the resonant wind speed of wind-induced vibration or galloping start wing speed can be within the design wind speed. The wind-induced vibration and galloping of highrise building with aspect ratio $H/\sqrt{DB}=6$, side ratio D/B=1 to 2 at intervals of 1/4 D/B were investigated in smooth flow. For the reducing effect of wind-induced vibration of highrise building, rectangular-highrise building with corners cutting about side ratio D/B=2 were investigated. Experimental results show that in the smooth flow non corners-cutting cases have tendency of increasing wind-induced vibration and galloping vibration then corner-cutting section. Therefore, the wind-induced vibrations on rectangular-highrise buildings were reduced effectively by using corner cut method.

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A Construction of Aerodynamic Force Measurement System for Wind Tunnel Test of Yacht Sail and Aerodynamic Forces Measurement of Model Sail (요트세일의 풍동시험을 위한 공력 계측시스템 구축과 모형세일의 공력 계측)

  • Kim, Choul-Hee;Choi, Jung-Kyu;Kim, Hyoung-Tae
    • Journal of the Society of Naval Architects of Korea
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    • v.48 no.5
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    • pp.445-450
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    • 2011
  • In order to estimate a yacht sail performance, measuring system of aerodynamic forces acting on the yacht sail is constructed and experiments of flexible model sail are carried out at the medium-size subsonic wind tunnel of Chungnam National University. Experimental results for a flexible sail are compared with experimental and numerical results of fixed shape sail. In case of a fixed shape sail, lift and drag coefficients are rarely changed at all velocity conditions. However, those of the flexible sail are decreased as the incoming velocity is increased. These are understandably resulted from shape variations due to the flexible material. Therefore aero-elastic similarity should be more carefully considered in the model test rather than other similarities.