AutoCADAutodesk是由美国公司开发的通用计算机辅助设计(Computer Aided Design,CAD)软件,具有易于掌握使用方便、体系结构开放等优点 ,能够绘制二维图形与三维图形、标注尺寸、渲染图形以及打印输出图纸,目 前已广泛应用于机械、建筑、电子、航天、造船、石油化工、土木工程、冶金 、地质、气象、纺织、轻工、商业等领域。 AutoCAD2007是 Auto CAD系列软件的最新版本,与 Auto CAD先前的版本相比 ,它在性能和功能方面都有较大的增强,同时保证与低版本完全兼容

AutoCADAutodesk是由美国公司开发的通用计算机辅助设计(Computer Aided Design,CAD)软件,具有易于掌握使用方便、体系结构开放等优点 ,能够绘制二维图形与三维图形、标注尺寸、渲染图形以及打印输出图纸,目 前已广泛应用于机械、建筑、电子、航天、造船、石油化工、土木工程、冶金 、地质、气象、纺织、轻工、商业等领域。 AutoCAD2007是 Auto CAD系列软件的最新版本,与 Auto CAD先前的版本相比 ,它在性能和功能方面都有较大的增强,同时保证与低版本完全兼容

In this lecture, we will particularize the conservation principles presented in the previous lecture to the case in which the system of particles considered is a 2D rigid body. Mass Moment of Inertia In the previous lecture, we established that the angular momentum of a system of particles relative to the center of mass, G, was

A pendulum is a rigid body suspended from a fixed point (hinge) which is offset with respect to the body's center of mass. If all the mass is assumed to be concentrated at a point, we obtain the idealized simple pendulum. Pendulums have played an important role in the history of dynamics. Galileo identified the pendulum as the first example of synchronous motion, which led to the first successful clock developed

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

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

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

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)

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

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