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【习题】V2 导弹尾翼振动模态分析 ? / Modal Analysis of a V2 missile Blade ?
加分题,很简单。(5分以上者,就不用做了)
老规矩:贴出答案 +1 分, 贴出命令流 +3 分 (认真编辑)
题目在老外的网站上(略有窜改 )
http://www.andrew.cmu.edu/course/24-ansys/htm/v1_turbine.htm
Vibration #1: Modal Analysis of a Turbine
Introduction: In the area of dynamics and vibrations the natural frequencies of a structure is of great importance to determine whether a structure can withstand excitation from the surroundings. In this example, we will learn to model a turbine and then determine its first few natural frequencies.
Physical Problem: To determine the natural frequencies of the turbine shown in the figure. Modal analysis means the calculation of the natural frequencies of a mechanical system. It also involves the calculation of the mode shapes.
Problem Description:
We will model the turbine as a disk with blades fixed on it ('blisk'=bladed disk). The inner radius of the hub is 10 cm, outer radius is 40 cm, blade length is 20 cm, blade width is 5 cm, and the thickness is 2.5 mm
Material: Assume the structure is made of steel with modulus of elasticity E=210 GPa and has a Poisson ratio of 0.3 and density of 7.21e3 kg/cubic meter.
Boundary conditions: The blisk is fixed around the inner diameter of the disk.
Loading: The blisk is not loaded.
Objective: To determine first three family of modes.
To animate the mode shape of the first 3 modes.
You are required to hand in print outs for the above. You don't have to hand in the animation files but you will have to give at least 3 captured frames of the animation for each of the three modes. |
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