RRLC测定葡萄籽超临界CO2萃取液中的原花青素

用高分离度快速分离液相色谱法测定超临界葡萄籽萃取液中原花青素含量。色谱柱:ZorbaxXDB C18(4.6mm×50mm,1.8μm),柱温:40℃;流动相:1.5%乙酸甲醇-1.5%乙酸水(90:10,V/V);检测波长:280nm;进样量:5μL,流速:0.9mL/min。原花青素在0.60—3.6mg/mL(R2=0.9997)范围内峰面积与浓度呈良好线性关系,平均加标回收率为100.6%,RSD=1.07%(n=6)。方法简单、快速、准确、可靠,为原花青素含量测定提供一种新选择。     

撞击流中颗粒碰撞传热理论模型研究

建立了考虑颗粒接触面导热的颗粒碰撞传热模型,相应完善了气固两相撞击流理论模型,并对不同条件的撞击流干燥过程进行了模拟。计算结果与实验结果非常吻合,从而验证了所建模型的正确性。本文还分析了颗粒碰撞传热、加料方式以及喷嘴间距对撞击流干燥性能的影响规律。结果表明:在本文所涉及的撞击流干燥过程中,颗粒碰撞传热对干燥性能的影响并不明显;单边加料时颗粒物料的降水幅度及撞击流装置的干燥强度都明显大于双边加料的工况;喷嘴间距较大时,物料的降水幅度及装置的干燥强度均较大。     

基于Fluent的超高压撞击流乳化喷嘴的优化分析

高压液体通过喷嘴加速,形成高速射流,与相反方向的另一股射流相互撞击,发生强烈的相互作用,产生强烈的径向和轴向湍流速度分量以及狭窄的高压高速湍流区,在此区域内,相间或液滴间的碰撞互磨产生的挤压力和剪切力使流体被细化。本文从液体连续相撞击流的两个特征：微观混合和压力波动入手,逐一分析了撞击速度与微观混合、压力波动的关系,得出了压力波动与撞击流速度乱U0成正比关系,微观混合与U^3 0成正比的规律。同时,用流体模拟软件Fluent对喷嘴的结构和尺寸进行优化,并得出最合理的喷嘴结构和尺寸。模拟认为：在相同压力下,采用矩形槽,出口孔径为0．2mm,槽的深度为0．27mm的结构时撞击速度达到最大,并通过实验验证了这一结论。     

防护板尺寸对Whipple防护结构撞击损伤影响的实验研究

通过高速撞击实验,探讨了采用小尺寸防护板的可行性。实验中采用的Whipple结构由尺寸变化的1 mm厚防护板（前板）和尺寸固定的3 mm厚舱壁板（后板）组成,防护板与舱壁板间隔10 cm。防护板为边长分别为8、12、16和20 cm的方形2A12铝合金板,舱壁板为边长为20 cm的方形5A06铝合金板。实验过程中均采用直径为4 mm的铝合金球形弹丸,撞击速度为1.45~1.71 km/s。实验结果表明:Whipple防护结构在舱壁板被击穿的概率大于0.8的条件下和击穿概率为0的条件下的极限速度以及舱壁板临界击穿条件下的速度都与防护板尺寸无关;并且,防护板前后表面击穿孔的直径及击穿孔侧壁的倾斜角也与防护板尺寸无关;但是,在速度相同的条件下随着板尺寸的增大,防护板板面的最大挠度增大,而且,防护板挠曲面的凸凹方向也由单一的凹向变成凸凹方向交替出现;随着速度的增加和板尺寸的增大,防护板最大挠度的增量减小。     

过冷水滴撞击螺旋桨桨叶表面的数值模拟

本文介绍了某型螺旋桨在不同飞行状态下.求解桨叶水滴撞击特性的数值方法.该方法对桨叶运动模型进行简化,并在对绕桨叶运动的气流场计算的基础上,采用拉格朗日方法求解气流场中水滴运动方程,得到水滴运动轨迹.进而,确定了水滴对桨叶的撞击特性参数,为桨叶防冰系统设计提供条件.主要结论如下:(1)在巡航状态下,桨叶沿展向方向上总收集系数Em和局部收集系数β不断增大;(2)在爬升状态下,随着爬升高度H不断增大,飞行速度V0不断增大,水滴撞击在桨叶表面的范围有所增加,而且β随之增大;(3)随着水滴平均有效直径(MVD)的增大,水滴撞击在桨叶表面的范围明显增加同时,β在桨叶表面同一位置的值也随之增大.     

Landing gear noise control using perforated fairings

Landing gears of commercial aircraft make an important contribution to total aircraft noise in the approach configuration. Using fairings to shield components from high speed impingement reduces noise. Furthermore, perforating these fairings has been confirmed by flight tests to further enable noise reduction. Following an earlier fundamental study of the application of perforated fairings, a study has been performed to investigate and optimize the benefits of bleeding air through landing gear fairings. By means of wind tunnel tests, an aerodynamic and acoustic survey has been performed on a simplified generic main landing gear to explore the influence of （perforated） fairings on the lower part of the gear. The results show that for this specific case, the application of impermeable fairings reduces noise in the mid- and high frequency range by shielding sharp edged components from high velocity impingement. However, below 1 kHz the noise is shown to increase significantly. Application of the perforations is shown to diminish this low frequency increase whilst maintaining the reduction in the mid- and high frequency range. The aerodynamic and acoustic measurements point in the direction of the separated flow of the fairings interacting with the downstream gear components responsible for the low frequency noise increase. Bleeding of the air through the fairings reduces the large scale turbulence in the proximity of these components and hence diminishes the low frequency noise increase.     

超高速摄影用高强度铝合金转镜动态特性的研究

转镜型超高速摄影机的信息容量取决于转镜的材料和横截面形状.本文首次对超高速摄影用高强度铝合金转镜从理论和实验两个方面进行了系统研究.研究表明:高强度铝合金是超高速分幅摄影机转镜的理想材料;当铝转镜截面形状为正三角形、镜面尺寸为(17×32.5)mm²时,转速已达(50×10⁴)rpm,镜面尺寸为(33×24)mm²时,转速已达(40×10⁴)rpm.     

Mass Spectrometry of 2a, 4-Disubstituted 5-Benzoyl-2a, 3,4,5-tetrahydro-2-phenoxy-azeto [ 1,2-a ] [1,5 ] benzodiazepin - 1 （2H）-ones Under Electron Impact Ionization Conditions

The mass spectrometric fragmentation of 2a, 4-disubstituted 5-benzoyl-2a, 3,4, 5-tetrahydro-2-phenoxy-azeto[1,2-α] [ 1,5 ] benzodiazepin-I (2H)-ones has been investigated by means of mass-analyzed ion kinetic energy spectrometry under electron impact ionization conditions. All compounds tend to lose different moieties, such as phenoxy, phenoxy and H, and phenoxyketene. Both [ M^ - PhO ] and [ M^ - PhOH ] ions could further lose CO, and the [ M^ - PhOCH = C = O] ions could lose propene or styrene, PhCON, PhCOHN, and other fragments.     

Torsional impact response of a penny-shaped crack in a functional graded strip

The torsional impact response of a penny-shaped crack in a nonhomogeneous strip is considered. The shear modulus is assumed to be functionally graded such that the mathematics is tractable. Laplace and Hankel transforms were used to reduce the problem to solving a Fredholm integral equation. The crack tip stress field is obtained by considering the asymptotic behavior of Bessel function. Explicit expressions of both the dynamic stress intensity factor and the energy density factor were derived. And it is shown that, as crack driving force, they are equivalent for the present crack problem. Investigated are the effects of material nonhomogeneity and strip‘s highness on the dynamic fracture behavior.Numerical results reveal that the peak of the dynamic stress intensity factor can be suppressed by increasing the nonhomogeneity parameter of the shear modulus, and that the dynamic behavior varies little with the adjusting of the strip‘ s highness.     

长杆弹超高速侵彻半无限混凝土靶实验研究及开坑分析

随着超高速动能武器的发展,长杆弹超高速侵彻混凝土靶机理成为当前的研究热点。为了探究长杆弹超高速侵彻混凝土靶的侵彻机理和开坑规律,本文中开展了TU1铜、Q235钢两类长杆弹以初速度1.8～2.4 km/s正侵彻强度26.5、42.1 MPa混凝土靶的超高速实验。结合文献和本文中的实验数据,对开坑直径和开坑体积进行量纲分析,基于开坑截面的弓形形貌几何关系,得到了开坑深度预测公式。结果表明:靶面开坑尺寸明显大于中低速侵彻时的靶面开坑尺寸,在分析侵彻机理的过程中不能忽略开坑阶段;弹体发生严重的长度缩短,直至最后完全侵蚀,弹洞半径明显大于弹体半径,说明长杆弹超高速侵彻半无限混凝土靶属于半流体侵彻机制。另外,在超高速侵彻条件下:弹体长度是影响侵彻深度的最主要参数;侵彻深度随弹体长度和密度的增大而增大,受弹体强度影响不大。