All Matches

Solution Library

Expert Answer

Textbooks

Search Textbook questions, tutors and Books

Oops, something went wrong!

Change your search query and then try again

Result Not Found

Books FREE
Tutors
Study Help
Hire a Tutor
AI Study Help New

Search
Sign In
Register

study help
engineering
mechanical vibration analysis

Questions and Answers of Mechanical Vibration Analysis

Suppose that for the two degree-of-freedom system of Figure 6.54 we obtain the data: \(f_{1}=4 \mathrm{~Hz}, f_{2}=\) \(10 \mathrm{~Hz}, f_{3}=8 \mathrm{~Hz}\), and \(m_{1}+m_{2}=20 \mathrm{~kg}\).
Since liquids have damping characteristics, suggest possible equivalent mechanical models for a sloshing liquid that includes damping.
Suppose a container with interior fluid is in an aircraft. The aircraft leaves on its flight with full tanks and arrives at its destination with almost empty tanks. How could this fact be
Suppose a container with interior fluid is in a spacecraft in orbit around the Earth. What additional considerations need to be incorporated in the equivalent mechanical model?
In Example 6.23, solve for \(\theta(t)\) analytically for the case \(g Example 6.23 Pendulum Forced at the Base Figure 6.60 is a sketch of a pendulum rotating about a vertically translating point.
Derive Equations 6.154 and 6.155 using Newton's second law of motion. Le+(+9) sin=0. (6.154)
For a two disk torsional system (see Figure 6.81) with its two ends fixed to walls, follow the procedure of Example 6.24 to evaluate the two approximate frequencies of oscillation. Explain the
How would Rayleigh's quotient need to be altered for an unrestrained system? Apply the method to a general two degree-of-freedom undamped system in unrestrained rectilinear motion.
Derive Equation 7.4,\[\frac{\partial}{\partial x}\left[T(x) \frac{\partial y}{\partial x}\right]+f(x, t)=m(x) \frac{\partial^{2} y}{\partial t^{2}}\]using Newton's second law of motion.
Solve for the string response, Equation 7.27, given the following initial conditions:(a) \(y(x, 0)=0, \dot{y}(x, 0)=g(x)\)(b) \(y(x, 0)=\sin \pi x / L, \dot{y}(x, 0)=0\)(c) \(y(x, 0)=0, \dot{y}(x,
Derive the expression for the tension required in a simply supported transmission line modeled as a string of length \(l\) and linear density \(ho\), such that its fundamental frequency for
A string is stretched between \(x=0\) and \(x=L\) and has a variable density \(ho=ho_{0}+\varepsilon x\), where \(ho_{0}\) and \(\varepsilon\) are constants. The initial displacement is \(f(x)\), and
Consider the uniform string with constant mass per unit length \(m\), constant tension \(T\), and length \(L\), shown in Figure 7.36. One end of the string is fixed, and the other end is constrained
Consider the uniform string with constant mass per unit length \(m\), constant tension \(T\), and length \(L\) shown in Figure 7.37. One end of the string is fixed, and the other end is attached to a
Consider the uniform string with constant mass per unit length \(m\), constant tension \(T\), and length \(L\) shown in Figure 7.38. One end of the string is fixed, and the other end is attached to a
Consider the uniform string with constant mass per unit length \(m\), constant tension \(T\), and length \(L\) shown in Figure 7.39. One end of the string is attached to a mass \(M\) and the other
Consider the fixed-fixed uniform string made of two sections shown in Figure 7.40. The left section of the string has a constant mass per unit length \(m\), and the right section of the string has
Plot the displacement response of the string in Figure 7.36 at \(x=L\) as a function of time if the initial displacement is \(y(x, 0)=0.05 x / L\) and the initial velocity is zero. m, L, T x y(x,t)
Plot the displacement response of the string in Figure 7.36 at \(x=L\) if the string is initially horizontal and is subject to the sinusoidal input force at \(x=L, F(t)=F_{0} \sin \omega_{f} t\). Use
Plot the displacement response of the string in Figure 7.38 at \(x=L\) as a function of time if the initial displacement is \(y(x, 0)=0.05 x / L\) and the initial velocity is zero. The orthogonality
Consider a system consisting of discrete masses connected by springs in series as shown in Figure 7.41. Derive the equation of motion for mass \(m_{i}\) using Newton's second law, arrange the
Derive Equation 7.32. [{[(EA)))]de ]}] EA(x)- -m(x). Su dx + [(EA(x)) bu] * } d dt = 0. (7.32)
For the uniform fixed-fixed beam in longitudinal vibration shown in Figure 7.42 derive the expressions for the natural frequencies and the mode shapes. Sketch the first three modes. x m, EA L Figure
For Equation 7.37, solve for the constants \(A_{r}\) and \(B_{r}\) by satisfying the initial conditions. M8 M8 u(x,t) = C, sin 3x(A, sin wrt + B+ cos wrt) 2 (2-1) sin -x mL 2L XA, sin (2-1) EA 2L m
Complete the solution of Example 7.2 for the modes and the complete solution. Example 7.2 Axial Vibration of Uniform Beam with Elastic Boundary Consider the axially vibrating beam shown in Fig- ure
Consider the free axial motion of a beam with the elastic boundary conditions of Example 7.2, and solve for the first four natural frequencies, modes, and the complete solution, for the following
An unrestrained beam lies on a horizontal and smooth surface and at \(t=0\) is forced at one end by \(F(t)\), as shown in Figure 7.43. Derive the general response for any forcing function using the
Find the response of a uniform beam clamped at \(x=0\) and free at \(x=L\) subjected to the longitudinal force,\[ f(x, t)=F_{o} \delta[x-(L-\varepsilon)] u(t) \]
Derive the natural frequencies and mode shapes of the longitudinally vibrating uniform beam of Figure 7.44. Sketch the first three mode shapes. What will change in the analysis if the beam is
A cantilever beam has its free end stretched uniformly so that the original length \(L\) becomes \(L_{0}\), and then it is released at \(t=0\), as shown in Figure 7.44. Begin with the general
Consider the stepped shaft made of the same material of density \(ho\) and modulus \(E\), shown in Figure 7.45. Determine the characteristic equation for the natural frequencies of the system as it
Consider the uniform beam shown in Figure 7.46. Solve for the lowest natural frequency of axial motion of the steel beam given the following parameter values: \(E=210 \mathrm{GN} / \mathrm{m}^{2},
Solve for the first three modes and frequencies of the nonuniform longitudinally vibrating beam of Figure 7.47 beginning with the known equation of motion. The following properties hold:\[
Consider the longitudinally vibrating uniform beam shown in Figure 7.48. One end of the beam is fixed and the other end is free with an attached concentrated mass \(M\). Derive the frequency
Derive the orthogonality condition for the eigenfunctions of the beam shown in Figure 7.48. x L m, EA M Figure 7.48: Axially vibrating cantilever beam fixed at one end with a point-mass at the other
Consider the longitudinally vibrating uniform beam shown in Figure 7.49. The ends of the beam are supported by linear springs with stiffnesses \(k_{1}\) and \(k_{2}\). Derive the frequency equation,
Consider the two identical longitudinally vibrating uniform beams shown in Figure 7.50 connected by a linear spring. Derive the frequency equation, the first three natural frequencies, and plot the
Plot the response of the concentrated mass in Figure 7.48 due to the initial displacement \(u(x, 0)=\) \(0.02 x / L\) and zero initial velocity. x L m, EA M Figure 7.48: Axially vibrating cantilever
Consider a fixed-fixed uniform torsional beam with length \(L\), torsional rigidity \(G J\), and mass per unit length \(m\). Derive the frequency equation, the first three natural frequencies, and
The uniform shaft of Figure 7.51 is subjected to the torque \(T_{0} \sin \omega t\) at its free end. (a) Find the steadystate vibration response by solving the free vibration problem, including the
Complete the general solution for \(\theta(x, t)\), assuming the arbitrary initial conditions \(\theta(x, 0)\) and \(\dot{\theta}(x, 0)\).
Solve for the frequencies, the modes and the total response \(\theta(x, t)\) of the system for the cases:(a) \(I L=I_{D}\),(b) \(I L=10 I_{D}\),(c) \(I L=I_{D} / 10\).
Consider the stepped shaft consisting of two uniform segments of lengths \(L_{1}\) and \(L_{2}\), torsional rigidities \(G J_{1}\) and \(G J_{2}\), and mass moments of inertia per unit length
In the oil drilling industry, a drill-tube is used for well-boring. It is a tube of outer diameter \(D_{o}\) and inner diameter \(D_{i}\) and is made of steel of density \(ho\) and modulus of
Derive Equations 7.53 and 7.54. [GJ(x)0'(x)] = w1(x)0(x), (7.53) dx
A circular elastic shaft of length \(L\) has one end clamped and a rigid disk attached at the other end, as shown in Figure 7.53. If \(G\) denotes the modulus of rigidity, \(J\) the area polar moment
Derive the frequency equation, the first three natural frequencies, and plot the first three mode shapes of a clamped-clamped uniform beam undergoing transverse vibration.
Derive the frequency equation, the first three natural frequencies, and plot the first three mode shapes of a clamped-pinned uniform beam undergoing transverse vibration.
Derive the frequency equation, the first three natural frequencies, and plot the first three mode shapes of a clamped-uniform beam with a concentrated mass \(M\) at the free end undergoing transverse
Perform the necessary variations to derive Equation 7.62 . y [8GA(x) (0-4)] -m(x)- + p(x, t) by dx t + EI(x)- : ) + GA(2) (3/2/2-4) -k2(x)m(x)- - t EI(x) L (-)}]* -[{GA(x) ( x dt = 0.
Equations 7.63 and 7.64 are solved using the assumed solutions \(y(x, t)=Y(x) \exp (i \omega t)\) and \(\psi(x, t)=\Psi(x) \exp (i \omega t)\). Find the characteristic equation. a [GA(2) x 2 -m(x).
In Equations 7.67 and 7.68, eliminate \(y(x, t)\) and derive the governing equation for \(\psi(x, t)\). What physical motion does this equation govern? SGAx SGA (3) a y t m- +p(x,t) = 0 (7.67)
Derive the Bernoulli-Euler beam equation, Equation 7.74. State all assumptions. a SGA- m- t +p(x,t) = 0 (7.67)
For the simply supported uniform beam of Figure 7.54 undergoing transverse motion, derive the natural frequencies and the natural modes of vibration. Sketch the first three mode shapes. What will
For the transverse vibration of a simply supported uniform beam, solve for the transient response if the initial conditions are given by\[ y(x, 0)=B\left(\frac{x}{L}-3 \frac{x^{2}}{L^{2}}+2
A two-span uniform beam may be used as a simple model of a bridge. For this model, sketched in Figure 7.55 , derive the frequency equation. L L m, El Figure 7.55: Two-span continuous uniform beam.
The beam of Figure 7.56 is released and rotates as a rigid body and impacts at an angular speed of \(\Omega\) \(\mathrm{rad} / \mathrm{s}\). Assume that upon impact the beam latches onto the support
Determine the characteristic equation for the transverse vibration of a beam that is pinned at one end and free at the other end.
List the boundary conditions for the transversely vibrating beams of Figures 7.57 and 7.58. L m, El M Figure 7.57: Transversely vibrating beam with end mass.
For the transversely vibrating beam of Figure 7.59 , find the modes and the first three natural frequencies of vibration. L -m, El M Figure 7.59: Transversely vibrating beam with end roller.
Complete the solution of Equation 7.97 for the initial conditions \(y(x, 0)=d(x)\) and \(\dot{y}(x, 0)=v(x)\). yr(x,t) =BY,(x) Fr(t) =Y,(x) cos(wyt - or), (7.97)
Derive Equation 7.102 beginning with Equation 7.101 . (ww) m(x)Y+(x)Y.(x)dx - [Y.(x) [EI(x) = da -[Y' (2) EI (2) dY, dY, da doc2 [[ d'Y, [Y-(*) [E1(2)]] dx +(x)EI(x)Y" (x)]. (7.101)
Derive Equation 7.106 starting with Equation 7.105. Y (2) d2 da2 EI(x) = dx dawr, r, 1, 2,.... = (7.105)
Fill in the steps in the derivation of Equation 7.110. Ely; (t) 5 dx4 =p;(t)(x). +c 1Y + m dt dt (7.110)
Solve Equation 7.113 for zero initial conditions and for each of the following forcing functions:(a) \(p(x, t)=u(t)\), where \(u(t)\) is the unit step function(b) \(p(x, t)=\sin \Omega t\)(c) \(p(x,
Derive the equation of motion and boundary conditions for a transversely vibrating beam using Hamilton's principle. Assume small deflections. Let \(I_{p}\) equal the mass moment of inertia per unit
Solve for the response of the cantilever beam sketched in Figure 7.61. m, L, EI Pcos Figure 7.61: Beam with harmonic end load.
In Example 7.7, solve for the case where \(t=\tau_{1} / 4\). Example 7.7 Evaluation of Arbitrary Constants and Vibration-Induced Stresses Continue Example 7.4 by evaluating the arbitrary con- stants
Find the response of a simply supported beam subjected to the external moment at \(x=L\),\[ p(x, t)=M(t) u^{\prime \prime}(x-L) \]
Derive the equation of motion for the transversely vibrating beam with axial force by applying Hamilton's principle.
Solve Equation 7.119 by setting the determinant of the coefficients equal to zero, resulting in a polynomial that is solved for the frequencies. Use the following parameter values: \(E=30 \times
Derive Equation 7.120. or 10 d da-4 - (pAw - k+)Y = 0, dY + -PA w + da4 (+) Y = 0. (7.120)
Derive Equation 7.122. Wy = + =(2) + ()* m m (7.122)
Discuss the modal participation factor for a vibrating beam that is subjected to loads as shown in Figure 7.62. Beam Load Load First Second case I case II mode mode Figure 7.62: Modal participation
Solve the equations of motion using the Laplace transform approach, where \(v(t)\) is the speed and \(F(t)\) is the force:(a) \(\dot{v}+2 v=F(t), v(0)=1, F(t)=0\)(b) \(2 \dot{v}+2 v=F(t), v(0)=0,
Solve the equations of motion using the Laplace transform approach:(a) \(\ddot{x}+3 \dot{x}+2 x=0, x(0)=1, \dot{x}(0)=0\)(b) \(2 \ddot{x}+5 \dot{x}+3 x=0, x(0)=1, \dot{x}(0)=1\)(c) \(\ddot{x}+2
Solve the equations of motion using the Laplace transform approach:(a) \(\ddot{x}+3 \dot{x}+2 x=u(t), x(0)=1, \dot{x}(0)=0\)(b) \(2 \ddot{x}+5 \dot{x}+3 x=e^{-3 t}, x(0)=1, \dot{x}(0)=1\)(c)
Solve the equations of motion using the Laplace transform approach:(a) \(\ddot{y}+2 \dot{y}+3 y=5 \cos 3 t, y(0)=3, \dot{y}(0)=4\)(b) \(4 \ddot{y}+5 \dot{y}+5 y=4 u(t), y(0)=1, \dot{y}(0)=1\), where
For the given transfer functions, find the response of the system due to the unit step input force \(F(t)=\) \(u(t)\) and zero initial conditions:(a) \(X(s) / \mathcal{F}(s)=1 /(s+2)\)(b) \(X(s) /
For the given transfer functions, find the response of the system due to the input force \(F(t)=\) \(2 \cos (3 t) u(t)\) and zero initial conditions:(a) \(X(s) / \mathcal{F}(s)=1 /(s+2)\)(b) \(X(s) /
Consider a system subjected to two input forces, as shown in Figure 4.30. Find the transfer functions, \(X(s) / \mathcal{F}_{1}(s)\) and \(X(s) / \mathcal{F}_{2}(s)\). Find the response \(x(t)\) due
A mass of \(m=50 \mathrm{~kg}\) is suspended by a spring attached to a rope that is wound around a drum with radius \(r=0.4 \mathrm{~m}\) and moment of inertia about the point of rotation \(I_{O}=45
Derive Equation 4.19:\[ v(t)=\frac{1}{\omega_{n}^{2}}\left[1-e^{-\zeta \omega_{n} t}\left(\cos \omega_{d} t+\frac{\zeta \omega_{n}}{\omega_{d}} \sin \omega_{d} t\right)\right] \]for \(t \geq 0\).
Assuming \(\zeta
Using the Laplace transform, solve\[ \ddot{y}+2 \dot{y}+y=F(t) \]where\[ F(t)=u(t-1)-2 u(t-2)+u(t-3) \]is in terms of unit step functions, and \(y(0)=0\) and \(\dot{y}(0)=0\).
Find the impulse response function of a system whose equation of motion is given by(a) \(\dot{x}+4 x=f(t)\)(b) \(\ddot{x}+4 x=f(t)\)(c) \(\ddot{x}+5 \dot{x}+4 x=f(t)\)(d) \(\ddot{x}+2
Find the impulse response function of a system whose transfer function is given by(a) \(G(s)=1 /(2 s+1)\)(b) \(G(s)=1 /\left(2 s^{2}+3 s+1\right)\)(c) \(G(s)=1 /\left(s^{2}+4 s+4\right)\)(d) \(G(s)=1
Find the response of each of the systems given below to arbitrary inputs, \(f(t)\) :(a) \(\dot{x}+4 x=f(t), f(t)=u(t)\)(b) \(\ddot{x}+4 x=f(t), f(t)=t, t \geq 0\)(c) \(\ddot{x}+5 \dot{x}+4 x=f(t),
Find the response of the undamped oscillator \(\ddot{x}+\) \(4 x=F(t) / m\) to each of the following forces per unit mass using the convolution integral:(a) \(F(t) / m=1-e^{-t}, t \geq 0\)(b) \(F(t)
Find the response of the damped oscillator \(\ddot{x}+\) \(2 \zeta \omega_{n} \dot{x}+\omega_{n}^{2} x=F(t) / m\), with \(\omega_{n}^{2}=4(\mathrm{rad} / \mathrm{s})^{2}\), to the forces per unit
Solve for the damped response beginning with the equation,\(x(t)=\frac{1}{m \omega_{d}} \int_{0}^{t} \sin \omega(t-\tau) \exp \left(-\zeta \omega_{n} \tau\right) \sin \omega_{d} \tau d \tau\).In the
The stepped disk in Figure 4.32 is subject to the moment\[ M(t)=1-e^{-t}, t \geq 0 \]The spring is unstretched when \(\theta=0\). Derive the equation of motion and solve for the response
Structures are sometimes subjected to very rapidly applied loads of extremely short duration. These types of loads are called blast or explosive loads. Consider how such a load time history may look.
Resolve Problem 19 including damping. Discuss the importance of damping by comparing the two results. Problem 19:Structures are sometimes subjected to very rapidly applied loads of extremely short
Solve for the response for all time of an underdamped oscillator that is driven by the forcing function shown in (a) Figure 4.34, and (b) Figure 4.35. Use the convolution integral. -2.0 -1.5 -1.0 1
Use Lagrange's equation to derive the equation of motion for the simple pendulum of Example 4.15, except here assume that the mass \(m\) is suspended on a rigid bar that is connected to the support
For Example 4.16 derive the equation of motion using \(x\) as the generalized coordinate. Then solve this equation with initial conditions \(x_{0}, v_{0}\) to find\[ x(t)=\frac{v_{0}}{\omega} \sin
Derive the equation of motion of Example 4.16 using Newton's second law of motion. Example 4.16 A Rolling Disk The disk on the inclined plane of Figure 4.15 is supported by two massless springs. It
For the problem of oscillator control, given by Equation 4.32, consider the specific governing equation\[ \ddot{x}+2 \zeta \omega_{n} \dot{x}+\omega_{n}^{2} x=\frac{A}{m} \cos \omega t+F_{\text
How does randomness of excitation alter the analyst's ability to evaluate structural response?

Showing 200 - 300 of 2655

1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
Last

Services

Sitemap
Fun
Definitions
Become Tutor
Study Help Categories
Recent Questions
Expert Questions

Company Info

Security
Copyrights
Privacy Policy
Terms & Conditions
SolutionInn Fee
Scholarship

Get In Touch

About Us
Contact Us
Career
Jobs
FAQ
Campus Ambassador

Secure Payment

Download Our App

© 2024 SolutionInn. All Rights Reserved