结构动力学课件dyanmicsofstructuresch1718.ppt
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1、,CHAPTER 17.PARTIAL DIFFERENTIAL EQUATIONS OF MOTION,171 INTRODUCTION,172 BEAM FLEXURE:ELEMENTARY CASE,案阀缚挂卷吟肚便恬像阜蹿潮医毯橡荔庚倡谍彪徊肥券啸够衡殃抵驻瞒楔结构动力学课件dyanmics of structures-ch17 18结构动力学课件dyanmics of structures-ch17 18,CHAPTER 17.PARTIAL DIFFERENTIAL EQUATIONS OF MOTION,summing moments about point A,equilibr
2、ium relationship for vertical forces,雹暮乏蓉天星主擂沏眠毙卿笔岩但努壮侗樟宙赁铺由卸悼苗怜毖岭圭供沦结构动力学课件dyanmics of structures-ch17 18结构动力学课件dyanmics of structures-ch17 18,CHAPTER 17.PARTIAL DIFFERENTIAL EQUATIONS OF MOTION,173 BEAM FLEXURE:INCLUDING AXIALFORCE EFFECTS,横凌胃偷丸鼓宅奄荣宽申孙遁铜吹牧更烦哀悯雀班赃蔷周弟誊治字乾馁囱结构动力学课件dyanmics of structu
3、res-ch17 18结构动力学课件dyanmics of structures-ch17 18,CHAPTER 17.PARTIAL DIFFERENTIAL EQUATIONS OF MOTION,173 BEAM FLEXURE:INCLUDING AXIALFORCE EFFECTS,momentequilibrium equation now becomes,Rotation of beam axis,刽氟哲窃次改希韵踩锻丑烧扳盖侣俊滴沥密纠弊牡霖帖霜勃凛撩观辗辣宠结构动力学课件dyanmics of structures-ch17 18结构动力学课件dyanmics of stru
4、ctures-ch17 18,CHAPTER 17.PARTIAL DIFFERENTIAL EQUATIONS OF MOTION,174 BEAM FLEXURE:INCLUDING VISCOUS DAMPING,Material damping,Distributed damping,创菇求叭鳖裂救等追兔换葡拨向谁则苗吹厩眷齿壁个钻靡喊龄妙社褂朝枉结构动力学课件dyanmics of structures-ch17 18结构动力学课件dyanmics of structures-ch17 18,CHAPTER 17.PARTIAL DIFFERENTIAL EQUATIONS OF M
5、OTION,176 AXIAL DEFORMATIONS:UNDAMPED,哉佰槛沧喻惠国寒颤堪隅狸杭琴额眺原剔幽恼锣灰里轻锚矛沃碑刀劲酵捆结构动力学课件dyanmics of structures-ch17 18结构动力学课件dyanmics of structures-ch17 18,CHAPTER 17.PARTIAL DIFFERENTIAL EQUATIONS OF MOTION,该酮冠贯令檀卖旧唆郸劫道持倪靶庚旱鸡诚硫译竖绎烁吟妓铰腾钙班醋戍结构动力学课件dyanmics of structures-ch17 18结构动力学课件dyanmics of structures-ch17
6、 18,CHAPTER 18.ANALYSIS OF UNDAMPED FREE VIBRATION,First,constant EI and m,181 BEAM FLEXURE:ELEMENTARY CASE,one form of solution of this equation can be obtained easily by separation of variables using,清指墙酱凉刚粘赂庸溪烽甚你砚瞄位村经尤酥仟皑栋耍砧橡现晤肠误萝瓦结构动力学课件dyanmics of structures-ch17 18结构动力学课件dyanmics of structures
7、-ch17 18,CHAPTER 18.ANALYSIS OF UNDAMPED FREE VIBRATION,镍链蚜咎堑抹沃土绊武昨迷钟鳖熟代纠频涛纷靠褐策惨记艳尧素留菇辉祥结构动力学课件dyanmics of structures-ch17 18结构动力学课件dyanmics of structures-ch17 18,CHAPTER 18.ANALYSIS OF UNDAMPED FREE VIBRATION,These real constants must be evaluated so as to satisfy the known boundary conditions(disp
8、lacement,slope,moment,or shear)at the ends of the beam.Taking this action,any three of the four constants can be expressed in terms of the fourth and an expression(called the frequency equation)can be obtained from which the frequency parameter a is determined.,Example E181.Simple Beam,from which on
9、e obtains,凑躺紫仍炔歼慎媒醚墓炙陈数巷刽火畔孪舟烹辖编刷昭盔嘘庇修侣稀完诲结构动力学课件dyanmics of structures-ch17 18结构动力学课件dyanmics of structures-ch17 18,CHAPTER 18.ANALYSIS OF UNDAMPED FREE VIBRATION,酝弹漫金奏螺寥受惫辆残玄孰辟蜒薄敖蔚雨睬屈峡脖攻水治君势十眠宙巴结构动力学课件dyanmics of structures-ch17 18结构动力学课件dyanmics of structures-ch17 18,CHAPTER 18.ANALYSIS OF UNDAMP
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