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731.
本文研究了几种基于不同类典型速度型有代表性的层流和湍流边界层积分方法,通过对这些方法的理论基础的考察以及对计算结果和实验结果的对比,讨论了它们的特点,评价了它们的适用性。 相似文献
732.
Zhongxian Shi Qijun Fu Renyang Zhao Zhengzhi Wang Jingxiu Wang Fei Wu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1982,2(11):229-232
A bright mass ejection appearing as a spray on the disk, associated with a 3b flare has been observed. A gap with a length of 2.5 × 104 km and a width of 2 × 104 km occurred between the flare and spray was observed. The intensity of the gap is about 1.6 times more intense than the undisturbed region. The spectral properties of the radio bursts corresponding to the flare and the spray are different. In addition, the flare and the spray are also different in their hard X ray emissions.Observation has not shown any relation between teh spray and the filament that existed previously in the active region. Perhaps the flare and the spray are produced simultaneously by the same mechanism. An observational model of the flare and the spray is shown in figure 3. 相似文献
733.
研究了二参数伽玛分布环境因子的估计。根据伽玛分布的特点,指数分布环境因子的定义,并考虑数据折算的方便,给出了伽玛分布环境因子的定义。根据此定义,用经典方法、贝叶斯方法和Fiducial 方法推证了环境因子的上、下限,并给出了一些近似式。 相似文献
734.
735.
To investigate the longitudinal motion stability of aircraft maneuvers conveniently, a new stability analysis approach is presented in this paper. Based on describing longitudinal aerodynamics at high angle-of-attack (a < 50 ) motion by polynomials, a union structure of two-order differential equation is suggested. By means of nonlinear theory and method, analytical and global bifurcation analyses of the polynomial differential systems are provided for the study of the nonlinear phenomena of high angle-of-attack flight. Applying the theories of bifurcations, many kinds of bifurcations, such as equilibrium, Hopf, homoclinic (heteroclinic) orbit and double limit cycle bifurcations are discussed and the existence conditions for these bifurcations as well as formulas for calculating bifurcation curves are derived. The bifurcation curves divide the parameter plane into several regions; moreover, the complete bifurcation diagrams and phase portraits in different regions are obtained. Finally, our conclusions are applied to analyzing the stability and bifurcations of a practical example of a high angle-of-attack flight as well as the effects of elevator deflection on the asymptotic stability regions of equilibrium. The model and analytical methods presented in this paper can be used to study the nonlinear flight dynamic of longitudinal stall at high angle of attack. 相似文献
736.
737.
As a key assembly in the 5-axis CNC machine tools, positioning precision of the A-axis directly affects the machining accuracy and surface quality of the parts. First of all, mechanical structure and control system of the A-axis are designed. Then, considering the influence of nonlin- ear friction, backlash, unmodeled dynamics, uncertain cutting force and other external disturbance on the control precision of the A-axis, an adaptive sliding mode control (ASMC) based on extended state observer (ESO) is proposed. ESO is employed to estimate the state variables of the unknown system and an adaptive law is adopted to compensate for the input dead-zone caused by friction, backlash and other nonlinear characteristics. Finally, stability of the closed-loop system is guaran- teed by the Lyapunov theory. Positioning experiments illustrate the perfect estimation of ESO and the stronger anti-interference and robustness of ASMC, which can improve the control precision of the A-axis by about 40 times. Processing experiments show that the ASMC can reduce the waviness, averaKe error and roughness of the nrocessed surface by 35.63%, 31.31% and 30.35%, respectively. 相似文献
738.
In micro-electro-mechanical system based inertial navigation system(MEMS-INS)/global position system(GPS) integrated navigation systems, there exist unknown disturbances and abnormal measurements. In order to obtain high estimation accuracy and enhance detection sensitivity to faults in measurements, this paper deals with the problem of model-based robust estimation(RE) and fault detection(FD). A filter gain matrix and a post-filter are designed to obtain a RE and FD algorithm with current measurements, which is different from most of the existing priori filters using measurements in one-step delay. With the designed filter gain matrix, the H-infinity norm of the transfer function from noise inputs to estimation error outputs is limited within a certain range; with the designed post-filter, the residual signal is robust to disturbances but sensitive to faults. Therefore, the algorithm can guarantee small estimation errors in the presence of disturbances and have high sensitivity to faults. The proposed method is evaluated in an integrated navigation system, and the simulation results show that it is more effective in position estimation and fault signal detection than priori RE and FD algorithms. 相似文献
739.
为了研究带止裂筋整体翼梁结构的裂纹扩展特性,采用ANSYS有限元软件对裂纹尖端应力强度因子进行数值计算,对缩比试验件进行疲劳裂纹扩展试验,当裂纹扩展到止裂筋前时进行剩余强度试验。结果表明:在梁缘条和蒙皮断裂情况下,止裂筋能够降低梁腹板上的应力强度因子幅值,对裂纹扩展起到拟制作用,其能够承担较大的静载荷从而实现破损安全设计,但是用止裂筋阻止疲劳裂纹扩展的效果并不显著;与梁弯曲产生的正应力相比,腹板上的剪应力不足以驱动Ⅱ型裂纹扩展。 相似文献
740.
本文通过对空间拦截运动学模型的线性化处理,提出了一种脉冲式末端导引规律,它既满足脱靶量指标,又使轨控发动机的燃料最省,且易于工程实现。仿真结果表明该导引律性能良好 相似文献