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An Experimental Investigation of Flow Induced Pressure Oscillations in Rectangular Cavities

机译:矩形腔流动诱导压力振荡的实验研究

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Wind Tunnel tests (WTT) were conducted measuring time average C_(PRMS) and mean C_p unsteady pressures acting on internal surfaces of rectangular cavities to build an understanding of the flow for free-stream speeds between U_∞ = 30 - 60m/s at Length-to-Depth (L/D) ratios; 0.5,0.8 at D = 380mm and 2 at D = 152mm. Root-Mean Square (RMS) of unsteady pressure C_p was computed to determine oscillatory peaks over variation of U_∞. Increasing length L as L/D = 0.5 - 0.8; showed an increase in intensity at all speeds. Decreasing depth D as L/D = 0.8-2 showed a shift in intensity from the walls to the floor at all speeds. Fluctuations were slightly less periodic from 30 - 60m/s, as increased speed reduced C_(PRMS) along x/L and y/D however increased C_p. Generally, as speed increases a cavities response changes, exhibiting progressively steeper gradients and larger pressure until a maximum respective to geometry. At this point, the cavity alters it's flow field to expel air faster. When mass outflow isn't enough, acoustic waves start to emit, becoming resonant at the onset velocity of the lower limiting frequency. Further work will investigate resonant modes and correlate their presence to the internal flow structure, observing effects of the absolute size and width.
机译:风隧道试验(WTT)进行测量时间平均C_(PRMS),并根据矩形腔的内表面的C_P非定常压力作用,以构建u_∞= 30-60m / s之间的自由流速度的流动的理解 - 深度(L / D)比率; D = 380mm,d = 152mm的0.5,0.8。计算不稳定压力C_P的根均线(RMS)以确定u_1的变化的振荡峰值。增加长度l为l / d = 0.5 - 0.8;显示所有速度强度的增加。减小深度d作为L / D = 0.8-2在所有速度下显示了从墙壁到地板的强度的偏移。随着30-60m / s的波动略小于30 - 60m / s,因为沿X / L和Y / D的增加的速度降低了C_(PRMS),但是增加了C_P。通常,随着速度增加腔响应变化,表现出逐渐陡峭的梯度和更大的压力,直到最大为几何形状。此时,腔体改变了它的流场以更快地驱逐空气。当质量流出不足时,声波开始发射,在下限频率的起始速度下变得谐振。进一步的工作将研究共振模式并将它们的存在与内部流动结构相关,观察绝对尺寸和宽度的效果。

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