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991.
992.
993.
采用共振拉曼光谱和完全活化空间自洽场方法研究了N,N-二甲基硫代乙酰胺在被激发至S3(ππ*)态后的衰减动力学. 指认了紫外吸收光谱和振动光谱. 获得了乙腈、甲醇和水溶剂中不同激发波长下的A带共振拉曼光谱,以探测Franck-Condon区域的结构动力学. 开展了CASSCF计算以确定低能单重激发态和锥形交叉点的电子激发能和优化几何结构. 通过共振拉曼强度分析和CASSCF计算获得了结构参数、A带结构动力学和S3(ππ*)态衰减机制. 提出了主要衰减通道为3,FC(ππ*)→S3(ππ*)/S1(nπ*)→1(nπ*). 相似文献
994.
995.
In the research of parachute, canopy inflation process modeling is one of the most complicated tasks. As canopy often experiences
the largest deformations and loadings during a very short time, it is of great difficulty for theoretical analysis and experimental
measurements. In this paper, aerodynamic equations and structural dynamics equations were developed for describing parachute
opening process, and an iterative coupling solving strategy incorporating the above equations was proposed for a small-scale,
flexible and flat-circular parachute. Then, analyses were carried out for canopy geometry, time-dependent pressure difference
between the inside and outside of the canopy, transient vortex around the canopy and the flow field in the radial plane as
a sequence in opening process. The mechanism of the canopy shape development was explained from perspective of transient flow
fields during the inflation process. Experiments of the parachute opening process were conducted in a wind tunnel, in which
instantaneous shape of the canopy was measured by high velocity camera and the opening loading was measured by dynamometer
balance. The theoretical predictions were found in good agreement with the experimental results, validating the proposed approach.
This numerical method can improve the situation of strong dependence of parachute research on wind tunnel tests, and is of
significance to the understanding of the mechanics of parachute inflation process.
The project supported by the National Natural Science Foundation of China (10377006).
The English text was polished by Yunming Chen. 相似文献
996.
We examine the axisymmetric buckling of a generalized Kirchhoff cylindrical shell under an axial wrench. If the shell is non-linear elastic, we provide a boundary value problem amenable to the bifurcation theory of Poincaré. Using this theory we prove a non-uniqueness theorem and obtain the critical loads and critical states. In the hyperelastic case, by exploiting the variational character of the problem, a global existence and non-uniqueness theorem is also proved.
Sommario Viene esaminato un problema di buckling per un guscio cilindrico, del tipo di Kirchhoff generalizzato, sotto un carico ai bordi di trazione-torsione. Nel caso elastico non lineare, si perviene ad un problema ai valori al contorno, cui si può applicare la teoria delle biforcazioni di Poincaré. In tal modo si dimostra un teorema di non unicità della soluzione e si ottengono i punti di biforcazione e i carichi critici. Nel caso iperclastico, facendo ricorso all'aspetto variazionale del problema, viene dimostrato un teorema globale di esistenza e non unicità della soluzione.相似文献
997.
998.
Mixed-mode stress intensity factors and critical angles of cracks in bolted joints by weight function method 总被引:2,自引:0,他引:2
Summary Mechanical joints, such as bolted or riveted joints, are widely used in structural components. Reliable determination of
stress intensity factors for cracks in bolted joints is required to evaluate their safety and fatigue life. The weight function
method is an efficient technique to calculate stress intensity factors for various loading conditions by the stress analysis
of an uncracked model. In this paper, the mixed-mode stress intensity factors for cracks in bolted joints are analyzed by
the weight function method, and coefficients included in the weight function are determined by finite element analysis for
reference loadings. The critical angle at which mode I stress intensity factor becomes maximum is determined, and the effects
of the amount of clearance and crack length on the critical angle are investigated.
Received 28 February 2001; accepted for publication 22 June 2001
RID="
ID=" The authors are grateful for the support provided by a grant from the Korea Science & Engineering Foundation (KOSEF)
and Safety and Structural Integrity Research Center at the Sungkyunkwan University. 相似文献
999.
Sequential non-linear least-square estimation for damage identification of structures with unknown inputs and unknown outputs 总被引:1,自引:0,他引:1
The detection of structural damages real-time on-line, based on vibration data measured from sensors, is an important but challenging research topic, and it has received considerable attentions recently. Due to practical limitations, it is highly desirable to install as few sensors as possible in the structural health monitoring system, leading to incomplete measurements of structural responses and excitations. The traditional time-domain analysis techniques, such as the least-square estimation (LSE) method and the extended Kalman filter (EKF) approach, require that all the external excitations (inputs) be available, which may not be the case for most structural health monitoring systems. Recently, the adaptive sequential non-linear least-square estimate (SNLSE) method has been proposed for the on-line identification of structural damages. In this paper, we extend the SNLSE method to cover the general case with unknown (unmeasured) excitations (inputs) and unknown (unmeasured) acceleration responses (outputs) in order to reduce the number of sensors required in the structural health monitoring system, referred to as the SNLSE-UI-UO. Analytic recursive solutions for the new approach are derived and presented. The accuracy and effectiveness of the proposed approach have been demonstrated using the Phase I ASCE structural health monitoring benchmark building, a 5-degree-of-freedom non-linear hysteretic building model, and a 3-story steel frame finite-element model. Simulation results indicate that the proposed approach is capable of tracking the changes of structural parameters leading to the identification of damages. 相似文献
1000.