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本文应用染色液流动显示技术对后缘偏转喷流情况下76°/40°双三角翼前缘涡破裂位置的变化进行了观测,实验结果表明偏转喷流主要推迟与喷流方向相同一侧前缘涡的破裂,而使另一侧前缘涡破裂略有提前.随着喷流偏转角度的增大,喷流使两前缘涡破裂位置差逐渐增大.另外,随着模型攻角的增大,前缘涡涡核与双三角翼翼面的夹角逐渐增大,导致偏转喷流的作用逐渐减弱. 相似文献
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报道关于高温燃气自由喷流(热喷流)、燃气喷流/主流干扰流对气动热环境影响的实验研究结果. 其意义在于: 抽象出高超声速飞行器实际飞行时燃气喷流及其干扰流的物理模型, 为高超声速飞行器防热需求提供实验依据. 实验主流由脉冲风洞提供,燃气喷流用氢氧燃烧驱动路德维希管的方式产生. 利用脉冲风洞驱动段压力信号自动控制热气源的产生以保证风洞主流与燃气喷流同步, 利用氢气、氮气和氧气的不同比例实现燃气喷流的热力学相似. 实验技术上完成了高温燃气喷流系统的参数采集与系统状态标定; 实验内容上开展了压缩拐角平板模型的气动热实验研究, 通过实验比较了只有主流流场、只有热喷流流场和既有主流流场又有热喷流流场(即干扰流场)3种工况的热流分布. 实验研究发现,热喷流/主流相互干扰会对压缩拐角平板上某一范围内的气动热环境造成显著影响, 热流峰值较无喷流流场高出一个量级. 相似文献
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《力学学报》2012,44(2)
报道关于高温燃气自由喷流(热喷流)、燃气喷流/主流干扰流对气动热环境影响的实验研究结果.其意义在于:抽象出高超声速飞行器实际飞行时燃气喷流及其干扰流的物理模型,为高超声速飞行器防热需求提供实验依据.实验主流由脉冲风洞提供,燃气喷流用氢氧燃烧驱动路德维希管的方式产生.利用脉冲风洞驱动段压力信号自动控制热气源的产生以保证风洞主流与燃气喷流同步,利用氢气、氮气和氧气的不同比例实现燃气喷流的热力学相似.实验技术上完成了高温燃气喷流系统的参数采集与系统状态标定;实验内容上开展了压缩拐角平板模型的气动热实验研究,通过实验比较了只有主流流场、只有热喷流流场和既有主流流场又有热喷流流场(即干扰流场)3种工况的热流分布.实验研究发现,热喷流/主流相互干扰会对压缩拐角平板上某一范围内的气动热环境造成显著影响,热流峰值较无喷流流场高出一个量级. 相似文献
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采用风洞试验和数值模拟相结合的方法,对雷诺数Re=55 000条件下细长旋成体有、无横向喷流时大攻角非对称特性进行了分析.通过风洞试验发现了旋成体在法向和侧向进行喷流时其大攻角非对称气动特性与无喷流时的区别,通过数值模拟方法对几个典型工况下旋成体有、无横向喷流时的非对称气动特性进行了分析,揭示了喷流对旋成体非对称流动分离的影响.通过风洞试验发现当细长旋成体进行法向控制时无喷流、喷流位于迎风区和喷流位于背风区的旋成体表现出了不同的非对称流动特性:首先喷流位于迎风区时攻角范围在20°~40°之间有喷流和无喷流旋成体所产生的侧向力方向相反,攻角大于40°之后侧向力系数的方向发生了改变,与无喷流时的侧向力系数方向相同,但是其绝对值要比无喷流时的侧向力系数小.其次喷流位于背风区时攻角在15°~35°之间有喷流时的侧向力系数绝对值要明显比无喷流时大,在随后的40°~70°之间旋成体侧向力系数变化规律与无喷流的趋势相似.当细长旋成体进行侧向控制时由于沿侧向的喷流所产生的直接力使得攻角范围在0°~20°之间和大于45°时有喷流的旋成体侧向力系数绝对值要比无喷流时大,但是攻角在25°~40°之间时旋成体... 相似文献
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喷流干扰是高超声速飞行高精度控制的一种有效手段,研究者们以往大部分都主要集中于连续流条件下喷流干扰效应的机理研究,并给出了喷流干扰流场的典型结构,而稀薄流条件下喷流干扰特性的实验数据还十分匮乏.本文利用JFX爆轰激波风洞产生高超声速稀薄自由流,基于平板模型开展不同喷流压力和自由来流参数对横向喷流干扰特性影响的实验研究,采用高速纹影成像及图像处理技术,获得稀薄流条件下喷流干扰流场演化过程及流场结构的变化规律.相比于无喷流条件形成的流场,横向喷流与稀薄自由流相互作用形成的流场结构更为复杂,喷流压力由于受到稀薄来流的扰动,斜激波会短暂穿透喷流干扰流场并延伸至楔形体上部.喷流干扰流场内桶状激波的影响范围随着喷流压力的升高而逐渐变宽,位于三波点上游的斜激波空间位置不会随喷流压力的变化而改变,而位于三波点下游的弓形激波则向上游移动,当喷流压力过低时,桶状激波不会与其他两种激波交汇形成三波点.高超声速稀薄来流压力的降低同样会使桶状激波的影响范围变宽,弓形激波同样也会向上游移动,但基本不会对斜激波空间位置产生任何影响. 相似文献
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采用测压方法研究了矢量喷流对细长旋成体大迎角非对称流动的影响特性.实验结果表明:矢量喷流对细长旋成体大迎角非对称侧向力有明显的抑制作用,该抑制作用是通过喷流诱导作用,改变其空间绕流涡系结构的分布来实现的,但是矢量喷流的存在并不能改变大迎角机身空间绕流涡系的本质结构;随着迎角的增大,矢量喷流对细长旋成体大迎角非对称流动的影响区域不断前移,甚至影响到头部;随着喷流落压比的增加,矢量喷流对细长旋成体大迎角非对称侧向力的抑制作用加强,但当喷流落压比达到临界落压比后(即喷管出口处达到设计马赫数时),喷流影响作用将不会随喷流落压比的增加而改变. 相似文献
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《International Journal of Solids and Structures》2003,40(17):4501-4517
A unified mixed, higher-order analytical formulation has been presented in this paper to predict general buckling as well as wrinkling of a general multi-layer, multi-core sandwich plate having any arbitrary sequence of stiff layers and cores. Assumptions of thin stiff layers and anti-plane core, which are usually made in the analysis of sandwiches, have been eliminated in the present formulation. Displacements as well as the transverse stress continuities have been enforced in the formulation by incorporating them as the degrees-of-freedom. The modal transverse stresses have been obtained directly as eigen vectors and thus their separate calculations have been advantageously avoided. Two sets of mixed models have been proposed on the basis of individual layer as well as equivalent single layer (ESL) theories by selectively incorporating non-linear components of Green’s strain tensor. Solutions from the models have been shown to be in excellent agreement with the available three-dimensional elasticity solutions as well as with the available experimental results. It has been demonstrated that the ESL theories cannot accurately evaluate the overall buckling as well as the wrinkling loads of sandwiches. Limitations of the typical simplifying assumptions have also been highlighted. 相似文献
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The interfacial deformation and stability of two-(A-B) as well as three-layer symmetric (A-B-A) and asymmetric (A-B-C) pressure-driven flow of viscoelastic fluids has been investigated. Flow visualization in conjunction with digital image processing has been used to observe and measure the rate of encapsulation and interfacial stability/instability of the flow. Specifically, the encapsulation behavior as well as stability/instability of the interface and the corresponding growth or decay rate of disturbances as a function of various important parameters, namely, number of layers and their arrangement, layer depth ratio, viscosity and elasticity ratio as well as disturbance frequency, have been investigated. Based on these experiments, we have shown that the encapsulation phenomena occurs irrespective of the stability/instability of the interface and in cases when both encapsulation and instability occur simultaneously their coupling leads to highly complex and three-dimensional interfacial wave patterns. Moreover, it has been shown that the simple notion that less viscous fluids encapsulate more viscous fluids is incorrect and depending on the wetting properties of the fluid as well as their first and second normal stresses the reverse could occur. Additionally, in two- and three-layer flows it has been shown that by placing a thin, less viscous layer adjacent to the wall longwave disturbances can be stabilized while short and intermediate wavelength disturbances are stabilized when the more elastic fluid is the majority component. Furthermore, in three-layer flows it has been demonstrated that in the linear instability regime no dynamic interaction between the two interfaces is possible for short and intermediate wavenumber disturbances. However, in the nonlinear stability regime dynamic interactions between interfaces have been observed in this range of disturbance wavenumbers leading to highly chaotic flows. Finally, in the parameter space of this study no subcritical bifurcations were observed while supercritical bifurcations resulting in waves with a pointed front and a gradual tail were observed. 相似文献
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风机叶片噪声的有源消声研究 总被引:2,自引:0,他引:2
建立了风机转动时产生的动叶气动噪声和静叶干涉噪声的声学模型,推导了声功率的表达式,根据最小辐射声功率准则导出了有源消声控制方程,并探讨了次级声源的配置参数对消声效果的影响。 相似文献
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IntroductionThesubtropicalanticyclone(subtropicalhigh)overEast_Asiaregionisanimportantsynopticsysteminfluencingthisregion’swe... 相似文献
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This present work focuses on the surface characterization of reactor-thermoplastic-polyolefin copolymers (R-TPO) for automotive
applications to deduce an appropriate parameter as a measure of the surface stickiness behavior. Therefore, nanoindentation
experiments are performed and the well-known mechanical contact properties have been determined. Additional, it has been tried
to measure an adhesion force between the indenter tip and the material’s surface. The adhesion force has been measured as
negative force during unloading and is the tensile force needed to bring the indenter tip to the initial position. Moreover,
the verification and correction of the viscoelastic effects have been considered. 相似文献
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Rheological properties in shear flow are presented for four different polyethylene samples: a high density, a linear low density and two low density polyethylenes manufactured using different techniques. Tests have been performed with the aid of capillary types of instrument equipped with capillaries of various lengths at three different temperatures. End correction factors have been determined and true flow curves obtained. Swelling ratios for both unannealed and annealed samples have been determined as well as the shear rate and shear stress at which irregularities begin. In some cases generalized plots have been prepared and in all cases the rheological response is discussed in terms of molecular characteristics, in particular the average molecular weight, molecular weight distribution and degree of branching. 相似文献
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Cross-section optimization of tower crane lattice boom 总被引:2,自引:0,他引:2
This paper discusses the problem of cross-section optimization of tower crane lattice boom. The trapezoid cross section has
been analyzed. The triangular and rectangular cross sections have also been analyzed as special cases. Total mass of the construction
has been selected as the objective function. Optimization parameters have been determined by Lagrange’s multipliers method.
Criterion of stress is used as the constraint function. Numerical examples are performed by usage of the obtained theoretical
solutions. Those results were than compared with ones obtained by usage of finite element method based computer program. On
the base of the analysis that was carried out, the recommendations are given regarding the application of trapezoid, triangular
and rectangular cross sections of the lattice constructions. 相似文献
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The flow-field structure in the vicinity and in the wake of an isolated 3D roughness element has been studied. Different experimental
techniques have been coupled and supported by CFD simulation for a good understanding of the flow-field topology. The results
have shown strong flow-field similarities for different roughness elements. A model describing the flow structure and interaction
mechanisms has been proposed. This model is in good agreement with experimental and CFD results as well as the literature. 相似文献
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Comparison of the three-phase oil relative permeability models 总被引:3,自引:0,他引:3
A comparative study of seven different methods for predicting three-phase oil relative permeabilities in the presence of gas and water phases is presented. Predicted oil relative permeabilities from these correlations have been compared with published three-phase experimental data obtained in Berea sandstone core samples. Some of the correlations under study have been recently developed and have never been tested against the laboratory data.The comparison shows that the commonly used models such as Stones' often do not give accurate predictions of the experimental data. It is concluded that the recently developed models fit the experimental data as well as or better than the previously developed and widely used three-phase oil relative permeability models. 相似文献