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1.意外伤害(Unintentional Injury):突然发生的事件对人体所造成的肉体和精神上的伤害,原因包括物理、化学和生物等各种因素,是儿童致伤、致残、致死的主要原因之一 2.1985年美国国家儿童卫生与人类发展研究所(NICHD)学术会议对意外伤害的定义和分类进行标准化 3.国际疾病分类(ICD-10)将其列为单独一类疾病
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一、西方美学史的研究对象和范围 严格说,美学史应当是世界美学史,它应当既包括西方美学史,又包括东方美学史。但 时至今日,还没有出现一部世界美学史我们讲的西方美学史,只是世界美学史的一部分。 “西方”两字主要指欧洲各国,还有美国和俄国;它只是一个地域性的概念,不是政治概念。 西方古典美学史主要是欧洲美学史
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MATLAB语言是一种广泛应用于工程计 算及数值分析领域的新型高级语言,自1984 年由美国 Math Works公司推向市场以来, 历经十多年的发展与竞争,现已成为国际公 认的最优秀的工程应用开发环境。 MATLAB功能强大、简单易学、编程效率 高,深受广大科技工作者的欢迎
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Lecture D33: Forced Vibration Fosinwt m Spring Force Fs =-kx, k>0 Dashpot Fd =-ci, c>0 Forcing Fext Fo sin wt Newton's Second Law (mix =CF) mx+cx+kx= Fo sin wt =k/m,=c/(2mwn)
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一、斯威齐模型 二、也称为折弯需求曲线模型。 三、由美国经济学家斯威齐于1939年提出。 四、用于解释一些寡头市场上的价格刚性现象
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Lecture D32: Damped Free Vibration Spring-Dashpot-Mass System k Spring Force Fs =-kx, k>0 Dashpot Fd =-cx, c>0 Newton's Second Law (mx =EF) mx +cx+kx (Define)Natural Frequency wn=k/m,and
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In this lecture, we consider the problem of a body in which the mass of the body changes during the motion, that is, m is a function of t, i.e. m(t). Although there are many cases for which this particular model is applicable, one of obvious importance to us are rockets. We shall see that a significant fraction of the mass of a rocket is the fuel, which is expelled during flight at a high velocity and thus, provides the propulsive force for the rocket
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When the only force acting on a particle is always directed to- wards a fixed point, the motion is called central force motion. This type of motion is particularly relevant when studying the orbital movement of planets and satellites. The laws which gov- ern this motion were first postulated by Kepler and deduced from observation. In this lecture, we will see that these laws are a con- sequence of Newton's second law. An understanding of central
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In this lecture, we will consider how to transfer from one orbit, or trajectory, to another. One of the assumptions that we shall make is that the velocity changes of the spacecraft, due to the propulsive effects, occur instantaneously. Although it obviously takes some time for the spacecraft to accelerate to the velocity of the new orbit, this assumption is reasonable when the burn time of the rocket is much smaller than the period of the orbit. In such cases, the Av required to do the maneuver is simply the difference between the
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In this lecture, we will derive expressions for the angular momentum and kinetic energy of a 3D rigid body. We shall see that this introduces the concept of the Inertia Tensor. Angular Momentum We start form the expression of the angular momentum of a system of particles about the center of mass
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