船舶力学
船舶力學
선박역학
JOURNAL OF SHIP MECHANICS
2006年
6期
1-10
,共10页
张亮%程丽%李凤来%盛其虎%汪玉
張亮%程麗%李鳳來%盛其虎%汪玉
장량%정려%리봉래%성기호%왕옥
水动力系数%模型试验%壁面干扰%卵形体%阻塞效应
水動力繫數%模型試驗%壁麵榦擾%卵形體%阻塞效應
수동력계수%모형시험%벽면간우%란형체%조새효응
hydrodynamic coefficient%model test%wall interaction%oval%blocking effect
对长度-厚度比为7.0的二维扁卵形体近平壁面运动的水动力特性进行了研究.拖曳水池试验选择了六种不同的壁面间距,五个攻角状态,将卵形体模型安装在U形槽中,保证流场的二维特性.Reynolds数范围从5×105到2×106.根据无界流实验结果,在数据处理中消除测力天平的安装角误差.给出了水动力系数相对于间距、攻角的回归公式,并划分了三个典型的干扰区域:升力区、混合区、阻塞区.实验表明:即使对于钝尾物体,也存在类似机翼的升力效应,无界流中扁卵形体的升力线斜率小于二维平板机翼的相应值.当物体离壁面较远时,水动力系数随攻角线性变化,壁面影响随间距减小而增大;当物体离壁面很近时,出现排斥现象,水动力系数随攻角的变化呈非线性特征.与其它参数相比,在大部分试验状态下,运动速度对水动力系数的影响较小.
對長度-厚度比為7.0的二維扁卵形體近平壁麵運動的水動力特性進行瞭研究.拖抴水池試驗選擇瞭六種不同的壁麵間距,五箇攻角狀態,將卵形體模型安裝在U形槽中,保證流場的二維特性.Reynolds數範圍從5×105到2×106.根據無界流實驗結果,在數據處理中消除測力天平的安裝角誤差.給齣瞭水動力繫數相對于間距、攻角的迴歸公式,併劃分瞭三箇典型的榦擾區域:升力區、混閤區、阻塞區.實驗錶明:即使對于鈍尾物體,也存在類似機翼的升力效應,無界流中扁卵形體的升力線斜率小于二維平闆機翼的相應值.噹物體離壁麵較遠時,水動力繫數隨攻角線性變化,壁麵影響隨間距減小而增大;噹物體離壁麵很近時,齣現排斥現象,水動力繫數隨攻角的變化呈非線性特徵.與其它參數相比,在大部分試驗狀態下,運動速度對水動力繫數的影響較小.
대장도-후도비위7.0적이유편란형체근평벽면운동적수동력특성진행료연구.타예수지시험선택료륙충불동적벽면간거,오개공각상태,장란형체모형안장재U형조중,보증류장적이유특성.Reynolds수범위종5×105도2×106.근거무계류실험결과,재수거처리중소제측력천평적안장각오차.급출료수동력계수상대우간거、공각적회귀공식,병화분료삼개전형적간우구역:승력구、혼합구、조새구.실험표명:즉사대우둔미물체,야존재유사궤익적승력효응,무계류중편란형체적승력선사솔소우이유평판궤익적상응치.당물체리벽면교원시,수동력계수수공각선성변화,벽면영향수간거감소이증대;당물체리벽면흔근시,출현배척현상,수동력계수수공각적변화정비선성특정.여기타삼수상비,재대부분시험상태하,운동속도대수동력계수적영향교소.
The hydrodynamic characteristics of a 2D oval with length-thickness ratio 7.0 while moving near plane wall were presented.Towing-tank tests were conducted under six distinct wall clearances and five attack angles and the 2D characteristics of flow field were ensured by installing the oval model in a U-shape trough.The Reynolds numbers considered were in the range of 5×105 to 2×106 .Through corresponding measuring data in unbounded flow field,the installing angle error of balance to model was eliminated in data processing. The regressive formulae of hydrodynamic coefficients relative to clearances,attack angles were given.Three typical interaction regions were divided,defined as Lifting,Mixed and Blocking Region.The experimental results indicate that even for the blunt-end body,there exists lifting effect similar to wing, and the lift-curve slope of oval in unbounded field is smaller than that of 2D wing. When the wall clearance is large,hydrodynamic coefficients vary linearly with attack angle,and the influence of wall increases with the decreasing of clearance.While for small clearance, there appear repulsion phenomena, and the variation of coefficients with attack angle is nonlinear. The effect of velocity on hydrodynamic coefficients is small at most cases,compared with other factors.