粉蠹虫性信息素的不对称合成新方法

昆虫性信息素;粉蠹虫性信息素的不对称合成新方法     

钯催化脱羰反应研究及若干昆虫性信息表的合成

综述了基于钯催化脱羰端烯化反应的若干昆虫性信息素的合成。     

昆虫运动机理的研究

昆虫运动机理研究是一门交叉学科的前沿基础研究。旨在完善现有的空气动力学理论,为微机械设计寻找新思想、新概念。本文重点介绍目前在昆虫运动参数测量中的一些关键问题和研究进展情况,并对如何分析这些参数进行一些简单说明     

含呋喃环双酰肼类衍生物的合成、杀虫活性及3D-QSAR研究

为发现新的昆虫生长调节剂,经单取代苯基呋喃甲酰氯与取代苯甲酰肼反应得到22个未见文献报道的含呋喃环双酰肼类化合物,其结构均通过了IR,1HNMR和元素分析确认.初步生测结果表明,所有目标化合物对豆蚜(Aphisfabae)均有活性,部分目标化合物表现出较好或中等的杀幼虫活性.化合物Ia,Ib和Ic在药剂浓度为0.05%时,对豆蚜的死亡抑制率分别为81.8%,58.4%和52.2%,其中化合物Ia对若蚜的蜕皮和成蚜产雌能力具有一定的抑制作用.而大部分目标化合物在药剂浓度为0.1%,0.05%和0.001%时,对3龄粘虫(Mythimna separate)、棉红蜘蛛(Tetranchus urticae)和尖音淡色库蚊(Culex pipiens pallens)幼虫杀虫活性不明显.采用比较分子力场分析(CoMFA)方法,对22个化合物的杀蚜虫活性进行三维定量构效关系(3D-QSAR)研究.在CoMFA研究中,考察了不同力场和电荷下网格点步长对统计结果的影响.建立了三维定量构效关系CoMFA模型(q2=0.518,r2=0.936).CoMFA模型的立体场、静电场三维等值线图不仅直观地解释了结构与活性的关系,而且为后续优化该系列化合物提供了理论依据.     

Control for going from hovering to small speed flight of a model insect

The longitudinal steady-state control for going from hovering to small speed flight of a model insect is studied, using the method of computational fluid dynamics to compute the aerodynamic derivatives and the techniques based on the linear theories of stability and control for determining the non-zero equilibrium points. Morphological and certain kinematical data of droneflies are used for the model insect. A change in the mean stroke angle （δФ） results in a horizontal forward or backward flight; a change in the stroke amplitude （δФ） or a equal change in the down- and upstroke angles of attack （δα1） results in a vertical climb or decent; a proper combination of δФ and δФ controls （or δФ and δα1 controls） can give a flight of any （small） speed in any desired direction.     

A computational study of the wing–wing and wing–body interactions of a model insect

The aerodynamic interaction between the contralateral wings and between the body and wings of a model insect are studied, by using the method of numerically solving the Navier-Stokes equations over moving overset grids, under typical hovering and forward flight conditions. Both the interaction between the contralateral wings and the interaction between the body and wings are very weak, e.g. at hovering, changes in aerodynamic forces of a wing due to the present of the other wing are less than 3% and changes in aerodynamic forces of the wings due to presence of the body are less than 2%. The reason for this is as following. During each down- or up-stroke, a wing produces a vortex ring, which induces a relatively large jet-like flow inside the ring but very small flow outside the ring. The vortex rings of the left and right wings are on the two sides of the body. Thus one wing is outside vortex ring of the other wing and the body is outside the vortex rings of the left and right wings, resulting in the weak interactions.     

昆虫飞行——非常规空气动力学

<正> 许多证据表明,昆虫飞行的机理与飞机及直升机的机理大不相同。zanker&Gotz测出了被系住的果蝇所产生的瞬时力。并发现这些力不能用常规空气动力学理论来解释。这些力也是这些果蝇使用不一般的方法来产生升力的证据。 在飞机稳态飞行时,空气在机翼上方流动比下方快。这时绕机翼周围有一纯环流。正是具有附体环流的机翼在空气中的运动产生了升力。可是,如果机翼从静止开始加速,那么它必须移动比它本身宽度长几倍的距离,才会有环流绕流机翼而产生足够的升力以使飞机达到稳态飞行。这一现象叫做Wagner效应。     

昆虫是怎样飞行的

 简述昆虫翅的拍动运动及昆虫飞行的控制方式, 介绍昆虫飞行的空气动力学原理和人们对这些原理的认识过程.     

Flows around two airfoils performing fling and subsequent translation and translation and subsequent clap

The aerodynamic forces and flow structures of two airfoils performing “fling and subsequent translation“ and “translation and subsequent clap“ are studied by numerically solving the Navier-Stokes equations in moving overset grids. These motions are relevant to the flight of very small insects. The Reynolds number, based on the airfoil chord length c and the translation velocity U, is 17. It is shown that: (1) For two airfoils performing fling and subsequent translation, a large lift is generated both in the fling phase and in the early part of the translation phase. During the fling phase,a pair of leading edge vortices of large strength is generated; the generation of the vortex pair in a short period results in a large time rate of change of fluid impulse, which explains the large lift in this period. During the early part of the translation, the two leading edge vortices move with the airfoils;the relative movement of the vortices also results in a large time rate of change of fluid impulse, which explains the large lift in this part of motion. (In the later part of the translation, the vorticity in the vortices is diffused and convected into the wake.) The time averaged lift coefficient is approximately 2.4 times as large as that of a single airfoil performing a similar motion. (2) For two airfoils performing translation and subsequent clap, a large lift is generated in the clap phase. During the clap, a pair of trailing edge vortices of large strength are generated; again, the generation of the vortex pair in a short period (which results in a large time rate of change of fluid impulse) is responsible for the large lift in this period. The time averaged lift coefficient is approximately 1.6 times as large as that of a single airfoil performing a similar motion. (3) When the initial distance between the airfoils (in the case of clap, the final distance between the airfoils) varies from 0.1 to 0.2c, the lift on an airfoil decreases only slightly but the torque decreases greatly. When the distance is about lc， the interference effects between the two airfoils become very small.