📄 mechanics of a tuned mass damper.m
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% This m-file shows the frequency response functions of a structure% (represented by its first mode) with and without a % tuned mass damper (TMD) tuned to its resonant frequency.%% The input parameters to the m-file are % the natural frequency of the structure, the mass% of the structure, the mass ratio of the tMD to that of% the structure, and the damping ratio of the TMD, as % shown below:%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% Define the parameters of the structure and TMD:w=2*pi*40; % mechanical resonaceM=10; %Kg. mass of the first modezeta=0.005; % damping ratio of the structure% Note that for numerical purposes a very small structural % damping ratio of 0.5% is assumed. If your structure has a higher% damping ratio, replace 0.005 in zeta to that of your% structural damping ratio, e.g. 0.02 for 2% damping ratio.b=0.1; %mass ratio of TMD to structure (m/M)zeta_tmd=0.3; % damping ratio of the TMD%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%The equations of motion, in Laplace domain, for a mass (M) %spring (K) system (resemblingthe first mode of a %structure) equipped with a tuned-mass-damper (m-c-k) is:%% |Ms^2+cs+(K+k) -(cs+k)||x | |F| % | || |=| |% |-(cs+k) ms^2+cs+k||x_tmd| |0|%%where s is the Laplace variable, F is the force disturbing %the structure, x is the displacement of the structure, and %x_tmd is the displacement of the mass of the tuned-mass_damper.%%Solving the above equation of motion for x results in the %transfer function% x (ms^2+cs+k)% ----------- = -----------------------------------% F (Ms^2+K)(ms^2+cs+k)+ms^2(cs+k)% where x displacement of the structure subject to% the disturbance force F. Note that without% the absorber m=0 the transfer function is that of the% original structure, i.e.,% x 1% ----------- = ----------% F (Ms^2+K)% Run the m-file with various damping ratios for the TMD and observe% that for very small damping ratios, the sturctural mode, splits into% two modes. The higher the mass ratio m/M, the higher the% spread between the two new splitted modes.%% Very small damping ratios are not suitable when the% objective of using TMD is adding damping to the structure. However% very small damping ratios are good when the goal is vibration % absorption, i.e., lowering the effect of forced vibration at a certain% frequency such as the rpm of a motor installed on a structure.K=M*w^2; %stiffness of the structure % assuming modal mass is M Kg num_structure=[1]; % transfer function of the structure disp/(static disp.)den_structure=[M zeta*2*sqrt(K*M) K];freq=10:.5:100; % frequency range of interestmag_structure=bode(num_structure,den_structure,2*pi*freq);m=b*M; %kg, mass of the TMDw_tmd=w; % natural frequency of the TMD is set equal to the structurek=m*w_tmd^2; % stiffness of the TMD is calculated so that natural % frequencies of TMD is the same as that of %the structurec=zeta_tmd*2*sqrt(k*m); % damping coefficient of the TMDnum=[m c k]; % transfer function of the structure with TMDden=conv([M 0 K],[m c k])+ [0 m*c m*k 0 0];mag=bode(num,den,2*pi*freq);plot(freq,20*log10(mag_structure),'-b',freq,20*log10(mag),'--m')legend('structure', 'structure+TMD')xlabel('Frequency, Hz');ylabel('Magnitude of x/F');title('FRF of displacment/Force with and without a TMD');
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