空气动力学学报
空氣動力學學報
공기동역학학보
ACTA AERODYNAMICA SINICA
2015年
4期
542-547
,共6页
脉动风%附加质量%气动阻尼%Hilbert-Huang 变换
脈動風%附加質量%氣動阻尼%Hilbert-Huang 變換
맥동풍%부가질량%기동조니%Hilbert-Huang 변환
fluctuating wind%added mass%aerodynamic%Hibert-Huang Transform
自振频率低且自重较轻的大跨度屋盖等结构体系在脉动风作用下发生振动时,附加质量及气动阻尼对其振动特性有重要影响,需通过对实验数据的准确识别研究其变化规律。基于 Hilbert-Huang 变换,在 IIR 带通滤波的基础上对输出信号进行经验模态分解,并对各自由度方向同步作随机减量处理得到所需模态阶次的自由衰减信号,进而求解频率、阻尼比及振型。数值算例表明,该方法可以有效抑制噪声影响,并准确提取不同阶次的模态参数。在此基础上,根据振型相似的原则对一肋环型索穹顶结构的附加质量及气动阻尼进行了识别,得出了这两个参数相比于静止空气环境以及随风速的变化规律。
自振頻率低且自重較輕的大跨度屋蓋等結構體繫在脈動風作用下髮生振動時,附加質量及氣動阻尼對其振動特性有重要影響,需通過對實驗數據的準確識彆研究其變化規律。基于 Hilbert-Huang 變換,在 IIR 帶通濾波的基礎上對輸齣信號進行經驗模態分解,併對各自由度方嚮同步作隨機減量處理得到所需模態階次的自由衰減信號,進而求解頻率、阻尼比及振型。數值算例錶明,該方法可以有效抑製譟聲影響,併準確提取不同階次的模態參數。在此基礎上,根據振型相似的原則對一肋環型索穹頂結構的附加質量及氣動阻尼進行瞭識彆,得齣瞭這兩箇參數相比于靜止空氣環境以及隨風速的變化規律。
자진빈솔저차자중교경적대과도옥개등결구체계재맥동풍작용하발생진동시,부가질량급기동조니대기진동특성유중요영향,수통과대실험수거적준학식별연구기변화규률。기우 Hilbert-Huang 변환,재 IIR 대통려파적기출상대수출신호진행경험모태분해,병대각자유도방향동보작수궤감량처리득도소수모태계차적자유쇠감신호,진이구해빈솔、조니비급진형。수치산례표명,해방법가이유효억제조성영향,병준학제취불동계차적모태삼수。재차기출상,근거진형상사적원칙대일륵배형색궁정결구적부가질량급기동조니진행료식별,득출료저량개삼수상비우정지공기배경이급수풍속적변화규률。
For the long-span roof structures which have relatively low frequency and light mass,the vibration property under the action of fluctuating wind is significantly influenced by the added mass and aerodynamic damping.The changing rule of these two parameters should be ex-tracted from exact identification method.Based on Hibert-Huang Transform theory,empirical mode decomposition method is applied on the output signal after IIR band pass filter.Then the random decrement technique is used synchronously on all the components of degrees of freedom to obtain the free decay signal of required mode,so the frequency,damping ratio and mode shape can be identified.The results of numerical example show that this method can restrain noise ef-fectively and extract the modal parameters of different order accurately.Taking the Geiger type cable dome as example,the added mass and aerodynamic damping under the action of fluctuating wind are identified according to the principle of highly similar mode shape,and the change law of these two parameters is also obtained compared with stationary air environment.