ME 429 Fall 2014 HW3 Solution You are expected to provide
Transcription
ME 429 Fall 2014 HW3 Solution You are expected to provide
ME 429 Fall 2014 HW3 Solution You are expected to provide clear explanation of each step of your solution, units, well annotated, scaled plots (title, axis labels, units, legend), not random hand sketches, source code attached to your solution if you use a software package in your calculations. Your grades are subject to these items as well as your calculations. Problem-1: Consider the single-DOF lumped mass-spring system with Coulomb damping shown below. g m = 12 kg k = 5 kN/m µ = 0.13 (a) If F(t) = 0 and an initial displacement of +35 mm is given to the mass m without any initial velocity, determine: (i) the response x(t) for any nth half-cycle and plot x(t) for the first 6 half-cycles (ii) the position and the time at which the mass stops (b) If F(t) = Fosin(40t) [N] and the amplitude of the steady-state oscillations of the mass is 30 mm, determine the amplitude of the harmonic force Fo applied to the mass. Solution: (a) This is the free vibrations case with δ = +35 mm. (i) The response x(t) for any nth half-cycle is formulated as: (1) Substituting the given values; (2) Note that since δ > 0, equals “-1” for odd n values (i.e. n = 1, 3, 5, …) and “+1” for even n values (i.e. n = 2, 4, 6, …). You can observe this phenomenon by looking at the drawn x(t) vs. t graph in the lecture notes. In addition, the time elapsed up to nth half-cycle is: (3) 1/5 Thus, the time elapsed between two subsequent half-cycles is: (4) 40 30 x(t) [mm] 20 10 0 -10 -20 -30 0 0.1 0.2 0.3 0.4 0.5 t [sec] 0.6 0.7 0.8 0.9 1 (ii) In order to determine the position and the time at which the mass stops, the maximum number of half-cycles that can be traveled until stopping should be determined first. The smallest integer n which satisfies the below inequality gives nmax: (5) Thus; nmax = 6 cycles Substituting nmax into Eqn. (3); tnmax = 0.92 sec The position at the end of the nth half-cycle is: (6) where 2/5 Substituting nmax into Eqn. (6); x(tnmax) = -1.73 mm %ME 429 Fall 2014 HW-3 Prob-1 Part-a Solution clc; clear all; close all; %System parameters m=12; %kg k=5000; %N/m wn=sqrt(k/m) %rad/s mu=0.13; g=9.81; %m/s^2 %Initial displacement delta=35*10^(-3); %m %The response of the system for n=1:6 for t=(n-1)*pi/wn:0.001:n*pi/wn if mod(n,2)==0 x=(delta-(2*n-1)*mu*m*g/k)*cos(wn*t)-mu*m*g/k; plot(t,x*10^3,'o'); hold on xlabel('t [sec]') ylabel('x(t) [mm]') grid on else x=(delta-(2*n-1)*mu*m*g/k)*cos(wn*t)+mu*m*g/k; plot(t,x*10^3,'o'); hold on xlabel('t [sec]') ylabel('x(t) [mm]') grid on end end end %Number of half-cycles traveled before the system stops n_max=ceil((delta-mu*m*g/k)/(2*mu*m*g/k)) %The time at which the mass stops tn_max=n_max*pi/wn %sec %The position at which the mass stops if mod(n_max,2)==0 x_max=(delta-2*n_max*mu*m*g/k)*10^3 %mm else x_max=-(delta-2*n_max*mu*m*g/k)*10^3 %mm end b) This is the forced vibrations case with X = 0.030 m. The amplitude of the steady-state x(t) is: (7) 3/5 where (8) since Ff = µmg. From Eqn’s (7) and (8); (9) Substituting the given values into Eqn. (9); Fo = 426.58 N Note that µmg/Fo = 0.036 < π/4. Problem-2: A structure showing hysteresis damping characteristics is subjected to a load of 3 kN which causes a static displacement of 1.5 cm. When the same structure is subjected to a harmonic force of amplitude 450 N at resonance, the resulting steady-state response amplitude is 25 cm. Determine: (a) the loss factor η (b) the steady-state response amplitude at ω = 0.4ωn as a result of the same harmonic force amplitude (c) the steady-state response amplitude at ω = 4ωn as a result of the same harmonic force amplitude Solution: (a) At static equilibrium; F = kx (10) Thus; k = 3000/0.015 = 200 kN/m At resonance where ω = ωn; (11) Thus; 4/5 (b) The steady-state response amplitude is: (12) At ω = 0.4ωn, thus, X = 2.68 mm (c) Substituting ω = 4ωn and the necessary numerical values into Eqn. (12); X = 0.15 mm 5/5