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[QUE/ME-02007]Node id: 3201page\(\newcommand{\Prime}{^\prime}\)Let \({\bf A, B,..}\) be objects with components written as \(\vec{A}=(A_1,A_2,A_3), \vec{B}=(B_1,B_2,B_3)\). Introduce \(\vec{A}\Prime=(A_1\Prime,A_2\Prime,A_3\Prime), \vec{B}\Prime=(B_1\Prime,B_2\Prime,B_3\Prime)\) etc. by means of equation \begin{equation}\label{EQ01} \begin{pmatrix}A_1\Prime\\A_2\Prime\\A_3\Prime\end{pmatrix} = R \begin{pmatrix}A_1\\A_2\\A_3\end{pmatrix} \end{equation} and with similar equations for other vectors.
Using the fact that the matrix \(R\) is orthodgonal matrix show that
- \({A}_i\Prime\vec{B}_i\Prime=A_i B_i\);
- If \(C_i\Prime=\epsilon_{ijk}A_j\Prime B_k\Prime\), then \(\vec{C}\Prime\) is given by an equation similar to \eqRef{EQ01}, where, of course, \(C_i=\epsilon_{ijk}A_j B_k\)
- The value of \( \vec{A}\Prime\cdot(\vec{B}\Prime\times\vec{C}\Prime)\) is independent of the matrix \(R\), if \(\det R=1\). What happens if \(\det R=-1\)?
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22-04-08 08:04:33 |
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[QUE/ME-02008]Node id: 3202page\(\newcommand{\Prime}{^\prime}\)For a four vector \(x=(\vec{x},x_4)\equiv(x_1,x_2,x_3,x_4)\), define a \(2\times2\) matrix \(M\) by \[M = x_\mu\sigma_\mu= x_4 + \vec{x}\cdot\vec{\sigma}\] where \(\sigma_4\) is \(2\times2\) identity matrix and \(\vec{\sigma}\) are Pauli matrices given by \begin{equation*} \sigma_1=\begin{pmatrix}0&1\\1&0\end{pmatrix},\quad \sigma_1=\begin{pmatrix}0&-i\\i&0\end{pmatrix},\quad \sigma_1=\begin{pmatrix}1&0\\0&-1\end{pmatrix} \end{equation*} Also define a matrix \(U\) by \begin{equation*} U = \cos\frac{\alpha}{2} + i\sin\frac{\alpha}{2}(\hat{n}\cdot\vec{\sigma}) \end{equation*} where \(\hat{n}=(n_1,n_2,n_3)\) is a unit vector.
- Show that \(U\) is unitary and \(\det U=1\).
- Prove that \(x_\mu = \frac{1}{2} Tr(\sigma_\mu M)\)
- Let \(M\Prime= U M U^\dagger\) Compute \(x_\mu\Prime \) and show that \begin{equation} x_4\Prime=x_4; \vec{x}\Prime=\vec{x}-\sin\alpha(\hat{n}\times\vec{x}) +(1-\cos\alpha)\hat{n}\times(\hat{n} \times\vec{x}) \end{equation}
In Newtonian mechanics,\(x_4\) can be identified with time.
Comment The last equation shows that to every rotation in three dimensions there are two \(SU(2)\) matrices given by \(\pm U\).
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22-04-08 08:04:40 |
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[QUE/ME-02010]Node id: 3204pageUsing definition of Levi-Civita epsilon symbol and Kronecker delta symbol to show that \begin{equation}\epsilon_{i\,j\,k}\,\epsilon_{k\,\ell\,m}\ =\ (\,\delta_{i\ell}\,\delta_{jm}\,-\,\delta_{im}\,\delta_{j\ell}) \end{equation} Use this identity to prove that \begin{equation}\vec{A}\times(\vec{B}\times\vec{C})=(\vec{A}\cdot\vec{C})\vec{B} -(\vec { A } \cdot\vec{B})\vec{C}.\end{equation}
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22-04-08 08:04:43 |
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[QUE/ME-02011]Node id: 3205pageUsing definition of Levi-Civita symbol, prove the following identities. \begin{eqnarray} \epsilon_{i\,j\,k}\,\epsilon_{i\,j\,k} \ &=&\ 6 \\ \epsilon_{i\,j\,k}\,\epsilon_{l\,j\,k} \ &=&\ 2\,\delta_{il} \\ \epsilon_{i\,j\,k}\,\epsilon_{l\,m\,k}\ &=&\ (\,\delta_{il}\,\delta_{jm}\,-\,\delta_{im}\,\delta_{jl}) \\ \epsilon_{i\,j\,k}\,\epsilon_{l\,m\,n}\ &=&\ \left(\begin{array}{ccc} \delta_{il}&\delta_{im}&\delta_{in}\\ \delta_{jl}&\delta_{jm}&\delta_{jn}\\ \delta_{kl}&\delta_{km}&\delta_{kn} \end{array} \right) \end{eqnarray}
Use result on \(\vec{A}\times(\vec{B}\times{\vec{C})}\) to give an alternate proof of identity (3) . |
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22-04-08 08:04:43 |
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[QUE/ME-02012]Node id: 3206pageShow that at least one eigenvalue of every rotation matrix is real. What are the ways in which all the three eigenvalues can be real? If the matrix has complex eigenvalues, show that they must come in complex conjugate pairs. |
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22-04-08 08:04:50 |
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[QUE/ME-02013]Node id: 3207page\(\newcommand{\Prime}{^\prime}\)Drive \(3\times 3\) rotation matrix corresponding to a rotation about axis \(\hat{n}\) by an angle \(\theta\) using the formula \begin{equation} \vec{x}\Prime = (\vec{x}\cdot\hat{n})\hat{n} - (\hat{n}\times\vec{x})\sin\theta - \hat{n}\times(\hat{n}\times\vec{x})\cos\theta. \end{equation}
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22-04-08 08:04:26 |
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[QUE/ME-12001] Circular OrbitsNode id: 3208pageConsider a particle moving in a spherically symmetric potential \[ V(r) = \frac{1}{2}m \omega^2 r^2 + \frac{\lambda^2}{2mr^2}\] Obtain condition for circular orbits for angular momentum \(L\ne0\).
When angular momentum is zero, \(L=0\) will there be a circular orbit? Assume angular momentum is zero, \(L=0\), and that the condition for circular orbit to holds, discuss possible types of motion that can take place. |
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22-04-08 08:04:25 |
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[QUE/ME-11002]Node id: 3210pageUnder what conditions can the problem of the motion of two charged particles in a uniform magnetic field be separated into the problem of the centre of mass motion and the relative motion problem of one body with reduced mass? |
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22-04-08 08:04:09 |
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[QUE/ME-11001]Node id: 3211pageFor a \(N\)- particle system, express the kinetic energy, the linear momentum, and the angular momentum of a system of \(N\) particles in terms of the Jacobi coordinates \begin{eqnarray} \vec{R}_j&=&\frac{m_1\vec{r}_1 + \ldots + m_j \vec{r}_j}{m_1+\ldots+m_j}-\vec{r}_{j+1}, \qquad j=1,\ldots,(N-1).\\ \vec{R}_N &=& \frac{m_1\vec{r}_1 + \ldots + m_N \vec{r}_N}{m_1+\ldots+m_N} \end{eqnarray} |
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22-04-08 08:04:03 |
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[QUE/ME-13001]Node id: 3212page[toc:0]
For a \(N\)- particle system, express the kinetic energy, the linear momentum, and the angular momentum of a system of \(N\) particles in terms of the Jacobi coordinates \begin{eqnarray} \vec{R}_j&=&\frac{m_1\vec{r}_1 + \ldots + m_j \vec{r}_j}{m_1+\ldots+m_j}-\vec{r}_{j+1}, \qquad j=1,\ldots,(N-1).\\ \vec{R}_N &=& \frac{m_1\vec{r}_1 + \ldots + m_N \vec{r}_N}{m_1+\ldots+m_N} \end{eqnarray} |
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22-04-08 08:04:53 |
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[QUE/ME-14002]Node id: 3270pageShow that the principal moments of inertia of a linear chain consisting of two kinds of atoms \(a,b\), with origin chosen to coincide with the centre of mass, is given by \[I_1=I_2=\frac{1}{M}\sum_{i\ne j}m_im_j \,d_{ij}^2, \qquad I_3=0.\] where the summation includes each pair of \(i,j\) atoms once and \(d_{ij}\)is the distance between atoms in the pair and \(M\) is the total mass. Verify that this gives correct answer for a triatomic molecule.
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22-04-08 08:04:55 |
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[QUE/ME-12002]Node id: 3273pageConsider a particle of mass \(\mu\) moving in a potential \[ V(r) = \frac{1}{2}\mu\omega^2 r^2 +\frac{\lambda^2}{2\mu r^2}. \] Does there exist a circular orbit for \(L=0\)? Assume \(L=0, E= \frac{25}{2}\mu\omega^2a^2\), \(\lambda=12\mu\omega^2\) Use initial conditions \[ r(t)\big|_{t=0} = 4a;\quad \dot{r}(t)\big|_{t=0} = 0 \text{ and } \dot{\theta(t)}\big|_{t=0}=0 \] solve the equations of motion and obtain \(r\), \(\theta\) as function of time. Describe the motion that takes place under conditions specified here.
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22-04-08 07:04:56 |
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[QUE/ME-12003]Node id: 3274pageJ.S.Plaskett's star is one of the most massive stars known at present. It is a double or a binary star, that is, it consists of two stars bound together by gravity. From spectroscopic studies it is known that the period of revolution of each component is 14.4 days; the velocity of each component is about 220 km/s; The orbit is nearly circular
(a) Argue that the masses of two stars are nearly equal and that they are nearly equidistant from the centre of mass of the system. (b) Compute the reduced mass and and the separation of the two components. |
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22-04-08 07:04:47 |
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[QUE/ME-12004]Node id: 3275pageComet Halley approaches the Sun to within 0.570 AU and its period is 75.6 years. How far from the Sun will this comet travel before it starts to return journey. Assume mass of Halley's comet is much smaller than the mass of the Sun. [Given : 1 AU $= 1.5 \times 10^{11}$ m, $G= 6.63\times10^{-11}$ N.m\(^2\) /kg\(^2\), Mass of Sun=\( 1.99\times10^{30}\) kg ]. |
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22-04-08 07:04:52 |
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[QUE/ME-12005]Node id: 3276page(a) A satellite of mass 2000 kg is to be put into a circular orbit around the earth of radius 1100 km. What is the minimum energy required? (b)What will the minimum energy required to transfer it to an elliptic orbit having minimum and maximum distances 1100km and 4100km? |
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22-04-08 07:04:22 |
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[QUE/ME12006]Node id: 3277pageConsider a particle of mass \(\mu\) moving in a potential \[ V(r) = \frac{1}{2}\mu\omega^2 r^2 +\frac{\lambda^2}{2\mu r^2}. \] (a) Find condition on energy \(E\) and angular momentum \(L\) for circular orbits to exist. (b) Does there exist a circular orbit for \(L=0\)? (c) Assume \(L=0, E= \frac{25}{2}\mu\omega^2a^2\), \(\lambda=12\mu\omega^2\) Use initial conditions \[ r(t)\big|_{t=0} = 4a;\quad \dot{r}(t)\big|_{t=0} = 0 \text{ and } \dot{\theta(t)}\big|_{t=0}=0 \] solve the equations of motion and obtain \(r\), \(\theta\) as function of time. Describe the motion that takes place under conditions specified here.
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22-04-08 07:04:12 |
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[QUE/ME-02023]Node id: 3279pageFind rotation matrix for a rotation by an angle \(\alpha\) about the axis \((1,2,1)\) where \(\cos\alpha=\frac{3}{5}, \sin\alpha =\frac{4}{5}\). |
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22-04-08 07:04:07 |
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[QUE/ME-08011]Node id: 3280pageFind rotation matrix for a rotation by an angle \(\alpha\) about the axis \(1,2,1\) where \(\cos\alpha=\frac{3}{5}, \sin\alpha =\frac{4}{5}\). |
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22-04-08 07:04:03 |
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[QUE/ME-12008]Node id: 3282pageConsider a particle of mass \(\mu\) moving in a potential \[ V(r) = \frac{1}{2}\mu\omega^2 r^2 +\frac{\lambda^2}{2\mu r^2}. \]
- Find condition on energy \(E\) and angular momentum \(L\) for circular orbits to exist.
- Does there exist a circular orbit for \(L=0\)?
- Assume orbital angular momentum \(L=0\), energy \(E= \frac{25}{2}\mu\omega^2a^2\), \(\lambda=12\mu\omega^2\) Use initial conditions \[ r(t)\big|_{t=0} = 4a;\quad \dot{r}(t)\big|_{t=0} = 0 \text{ and } \dot{\theta(t)}\big|_{t=0}=0 \] solve the equations of motion and obtain \(r\), \(\theta\) as function of time. Describe the motion that takes place under conditions specified here.
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22-04-08 07:04:00 |
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[QUE/CM-02033]Node id: 3284pageA bead of mass \(m\) slides on a frictionless wire under the influence of gravity and the shape of wire is parabolic with axis begin along the vertical upwards. The wire rotates about the its axis, (\(z\)- axis), with constant angular velocity \(\omega\). Take \(z^2= a\rho\) as equation of the parabola.
- Set up Lagrangian and obtain equations of motion.
- Obtain the Hamiltonian. Is theHamiltonian equal to energy? Is the Hamiltonian or energy or both areconstants of motion?
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22-04-08 07:04:40 |
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