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Journal of Hydronautics最新文献

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Duct effects on the dynamic fan characteristics of air cushion systems 风道对气垫系统风机动态特性的影响
Pub Date : 1977-06-30 DOI: 10.2514/3.48164
M. Hinchey, P. Sullivan
During dynamic operation of an air cushion system, the fan operating point as seen at the cushion does not move along a static characteristic. Instead, it moves on a loop. It is shown that loop type behavior can be predicted theoretically. The theory models the fan-duct-plenum system as a one dimensional acoustic vibration system. It uses the method of characteristics and a finite difference technique known as the method of specified time intervals to solve for the pressure and flow variations which occur along the duct during unsteady operation. Several practical situations where the loop behaviour may be of importance are discussed.
在气垫系统的动态运行过程中,在气垫上看到的风扇工作点并不沿着静态特性移动。相反,它在循环中移动。结果表明,循环型行为可以从理论上进行预测。该理论将风机-风筒系统建模为一维声振动系统。它采用特性法和有限差分技术(即指定时间间隔法)求解非定常运行过程中沿风道发生的压力和流量变化。讨论了几个实际情况,其中循环行为可能是重要的。
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引用次数: 5
Turbulent flow over a step with nonzero angle of inclination of the plates 在台阶上的湍流,板的倾斜角度非为零
Pub Date : 1977-04-01 DOI: 10.2514/3.48153
C. Liu, S. Foo, K. H. Ling
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引用次数: 1
Zero-Frequency Hydrodynamic Coefficients of Vertical Axisymmetric Bodies at a Free Surface 垂直轴对称体在自由表面的零频率水动力系数
Pub Date : 1977-04-01 DOI: 10.2514/3.63203
K. Bai
Yurnerical results are given for the addcd mass o l wrticnl nxisrmmetric br~dies piercing a free surface when Ihe fwql~cncy tends tu zeru. The numerical scheme employ a liniiu-ulumunl mrlhud which is based an the lheorv of calcutu o f vnr ia l ims. Spccifir. body geometries treated here are a family of sphuruids (oblate and pmlale sphemids) and a Fumily ~ r l vcrticlil circular cylinders with xarioos slenderness ratios. Thu cast when the free hurface plaw dues not intersect the center nC thr spheroid i* Iruatvd. Specifirally. Ihe heave and pitch rnoiionb are confidered. sincc clashiral annlj-tir resalts are availalde for thr hwag m d v n uf fl spheroid. ' l l ~ e present numerical resulls can he used in conncrclinn wilh ocean buoy or ocean platform motions hy ahwining lhat the hod) geomcrry i k c n cmnll cumpared wi th the warelenyth of rurfacr waves.
本文给出了在速度趋于零的情况下,所有非对称金属模具在自由表面上的附加质量的数值结果。数值格式采用了一种基于非线性计算理论的非线性模型。Spccifir。这里处理的身体几何形状是球形(扁圆球形和扁球形)和具有不同长细比的球形圆柱体。当自由面平面不与球面中心相交时,即为自由面平面。Specifirally。升降和俯仰的情况是保密的。由于碰撞效应的影响,我们已经得到了在全球面上的碰撞效应的结果。本文给出的数值结果可以用于与海洋浮标或海洋平台运动的关联,因为我们可以将CMNLL的几何特征与表面波的波长进行比较。
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引用次数: 6
Isothermal Flows in Water 等温水流在水中
Pub Date : 1977-04-01 DOI: 10.2514/3.63205
M. Rao, N. K. Purohit
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引用次数: 0
Practical Considerations Regarding Wing-in-Ground Effect Aircraft 关于地效机翼飞机的实际考虑
Pub Date : 1977-04-01 DOI: 10.2514/3.63200
E. Handler
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引用次数: 7
Aero/Hydrodynamic Forces and Moments on Self -Propelled Slender Bodies in Incompressible Flow 不可压缩流动中自行式细长体的气动/水动力力和力矩
Pub Date : 1977-04-01 DOI: 10.2514/3.63199
J. Schetz, Edward B. Daffant
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引用次数: 0
On the calculation of boundary layers along rotating cylinders 关于沿旋转圆柱方向边界层的计算
Pub Date : 1977-04-01 DOI: 10.2514/3.48154
J. S. Tennant, W. Johnson, D. Keaton
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引用次数: 13
Upright Sailing Craft Performance and Optimum Speed to Windward 直立帆船性能和最佳迎风速度
Pub Date : 1977-04-01 DOI: 10.2514/3.63201
H. Curtiss
A convenient geometric fnlutinn to the wind Irinnglc rel.alinnhip For a ailing crafl is de+elr~pcrl whwh is directly related to the armdynamic and hydrodynamic chnrncteriatics of Ihc cralt. Manimitiny rhc peed made good tu wiiideard is examined, and a relationship between the aerodynarnicr and hgdrodynamic nC the craft which bounds !he windward performance and is a necessav conditioir fur ~na~imum speed to windward is developed. A brief discussion of windward perfornunre tradeuffs is induded based vn thiv res~~lt.
一种方便的风振几何参数的计算方法,是一种与船体臂动力和水动力特性直接相关的几何参数计算方法。研究了使飞行器具有良好迎风性能的最小速度,并建立了飞行器的空气动力和水动力之间的关系,而空气动力和水动力是飞行器迎风性能的限制,是飞行器达到最大迎风速度的必要条件。对迎风性能的权衡进行了简要的讨论。
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引用次数: 5
IMPROVEMENT PLATE FOR SEMIBALANCED RUDDER 半平衡舵改进板
Pub Date : 1977-04-01 DOI: 10.2514/3.63207
Chang-yu Liu, Oag Beng Yoke, Tham Kwok Liang
The semi-balanced rudder has its fixed portion in the upper part of the leading edge and incorporates a balance area without introducing a vertical gap when the rudder is laid over. However, it necessarily incorporates a horizontal break between the top of the balance area and the lower edge of the fixed portion, which has an undesirable influence on its characteristics. An experiment has been carried out using a small plate to seal off the horizontal gap on rudder section shape NACA 0015, which was then tested in a low-speed wind tunnel with a test section of 30 x 30 cm. Surface pressures on the rudder for various degrees of deflection angle were measured. It was found that, at a large deflection angle, the improvement in normal force by sealing off the horizontal gap is approximately 6% and the steamline pattern is improved, added to which the large variation of the centre of pressure of the semi-balanced rudder may also be reduced.
所述半平衡舵在其前缘的上部有其固定部分,并且在放置舵时不引入垂直间隙的情况下包含平衡区。然而,它必然在平衡区域的顶部和固定部分的下缘之间包含水平断裂,这对其特性具有不希望的影响。采用小板密封NACA 0015型舵段的水平间隙,在30 × 30 cm的低速风洞中进行了试验。测量了舵在不同偏转角度下的表面压力。结果表明,在大偏转角下,封闭水平间隙法向力的改善约为6%,改善了蒸汽线型,并减小了半平衡舵压力中心的大变化。
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引用次数: 2
SCALING OF CAVITATION DAMAGE 空化伤害的缩放
Pub Date : 1977-01-10 DOI: 10.2514/3.63077
D. R. Stinebring
This investigation has focused on the initial stages of cavitation erosion using a ductile material in a flowing system employing water as the working fluid. The test models were 0.25-in. (0.635-cm)-diam zero-caliber ogives made of pure annealed aluminum. The damage was in the form of small round depressions in the model surface. In the formation of these pits, there was no material removal. For a range of velocities from 49 to 195 fps (14.9 to 59.3 m/sec), the pitting rate increased by approximately the sixth power of velocity. The average volume of the cavitation damage pits increased by the fifth power of velocity. A relationship between the volume of a pit and the absorbed bubble collapse energy was developed. The rate of total bubble collapse energy absorbed by the model then increases by the eleventh power of velocity. A plot of the distribution of absorbed collapse energies was generated for three flow conditions. The effect of cavitation number and air content of the working fluid were also major areas of investigation. A high-speed motion-picture study of cavity dynamics was undertaken to understand better some of the processes involved in cavitation damage. Lastly, the results of this study were compared with those of previous investigations of cavitation erosion.
本研究的重点是在以水为工作流体的流动系统中使用延展性材料进行空化侵蚀的初始阶段。测试模型为0.25-in。(0.635 cm)-直径零口径管由纯退火铝制成。损伤表现为模型表面出现小而圆的凹陷。在这些坑的形成过程中,没有物质被移除。在49 ~ 195 fps (14.9 ~ 59.3 m/sec)的速度范围内,点蚀率增加了大约6倍的速度。空化损伤坑的平均体积增加了5倍速度。建立了坑体体积与气泡崩塌吸收能量之间的关系。然后,模型吸收的总气泡崩溃能量的速率增加了速度的11次方。绘制了三种流动条件下的吸收塌缩能分布图。空化数和工质含气量的影响也是研究的主要领域。为了更好地了解空化损伤的一些过程,对空化动力学进行了高速电影研究。最后,将本文的研究结果与以往的空化侵蚀研究结果进行了比较。
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引用次数: 29
期刊
Journal of Hydronautics
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