大蹼铃蟾蛋白提取物对膀胱癌细胞株的抑制作用及对端粒酶的影响

目的探讨大蹼铃蟾蛋白提取物对膀胱癌细胞株的 抑制作用及对端粒酶的影响。方法采用肿瘤细胞培养方 法，检测大蹼铃蟾蛋白提取物对膀胱癌细胞株."%、/01’)+、 234/56的抑制作用；以.&-7’78&’9:02-方法检测大蹼铃 蟾蛋白提取物对膀胱癌细胞株端粒酶表达的影响。结果 大蹼铃蟾蛋白提取物表现出对膀胱癌细胞株有较强的抑制 作用；对膀胱癌细胞株端粒酶表达则无影响。结论大蹼铃 蟾蛋白提取物对多个膀胱癌细胞株具有直接细胞杀伤作用， 其作用机制不通过抑制端粒酶活性。

Flame imaging of gas-turbine relight

High-altitude relight inside a lean-direct-injection gas-turbine combustor is investigated experimentally by highspeed imaging. Realistic operating conditions are simulated in a ground-based test facility, with two conditions being studied: one inside and one outside the combustor ignition loop. The motion of hot gases during the early stages of relight is recorded using a high-speed camera. An algorithm is developed to track the flame movement and breakup, revealing important characteristics of the flame development process, including stabilization timescales, spatial trajectories, and typical velocities of hot gas motion. Although the observed patterns of ignition failure are in broad agreement with results from laboratory-scale studies, other aspects of relight behavior are not reproduced in laboratory experiments employing simplified flow geometries and operating conditions. For example, when the spark discharge occurs, the air velocity below the igniter in a real combustor is much less strongly correlated to ignition outcome than laboratory studies would suggest. Nevertheless, later flame development and stabilization are largely controlled by the cold flowfield, implying that the location of the igniter may, in the first instance, be selected based on the combustor cold flow. Copyright © 2010.

Microvortex generators applied to flowfield containing a normal shock wave and diffuser

The flow through a terminating shock wave and the subsequent subsonic diffuser typically found in supersonic inlets has been simulated using a small-scale wind tunnel. Experiments have been conducted at an inflow Mach number of 1.4 using a dual-channel working section to produce a steady near-normal shock wave. The setup was designed so that the location of the shock wave could be varied relative to the diffuser. As the near-normal shock wave was moved downstream and into the diffuser, an increasingly distorted, three-dimensional, and separated flow was observed. Compared with the interaction of a normal shock wave in a constant area duct, the addition of the diffuser resulted in more prominent corner interactions. Microvortex generators were added to determine their potential for removing flow separation. Although these devices were found to reduce the extent of separation, they significantly increased three-dimensionality and even led to a large degree of flow asymmetry in some configurations. Copyright © 2011 by Neil Titchener and Holger Babinsky.

大陆漂移与云南胡蜂的扩散分布

云南高原位于北纬21°9′～29°15′和东经97°39′～106°12′之间,总面积394000 km2 ,地质和气候、植被非常复杂。大 陆漂移和冰期的进退是影响昆虫起源和演替的一个重要原因。昆虫的祖先是起源于一个统一大陆,在这个大陆上共 同起源,共同进化,随着原始大陆的分离和漂移,把这些类群运载到各地,形成现今昆虫分布格局。昆虫的扩散是以中 心分布方式成环状向周围扩散的。云南胡蜂的祖先是来自冈瓦那古陆。有两支昆虫进入云南,其中一支来自喜马拉 雅山,另一支来自缅甸。冰期是导致南北生物互相混合和渗入的重要因素。胡蜂的特有类群是在冈瓦那古陆分裂之 后才发展起来的。其祖先最早是分布在原始古陆较狭窄的区域内。