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Gravitation Test - 72

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Gravitation Test - 72
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  • Question 1
    1 / -0

    Directions For Questions

    At points inside the earth the statements of gravitational field need to be modified. If one could drill a hole to the center of the earth and measure the force of gravity on a body at various distances from the center, the force would be found to decrease as the center is approached, rather than increasing as $$l/r^2$$. Qualitatively, it is easy to see why this should be so: as the body enters the interior of the earth (or other spherical body), some of the earth's mass is on the side of the body opposite from the centre of the earth and pulls the body in the opposite direction. Exactly at the center of the earth, the gravitational force on the body is zero.
    The magnitude of the gravitational constant $$G$$ can be found experimentally by measuring the force of gravitational attraction between two bodies of known masses $$m_1$$ and $$m_2$$ at the known separation for bodies of moderate size the force is extremely small, but it can be measured with an instrument called a torsion balance, invented by the Rev. John michell and first used for this purpose by Sir Henry Cavendish in $$1798$$. The same type of instrument was also used by Coulomb for studying forces of electrical and magnetic attraction and repulsion.

    ...view full instructions

    Consider the following statements about acceleration due to gravity on earth and mark the correct statement(s) :
    Solution
    Acceleration due to gravity at depth d,  $$g'=g(1-\dfrac{d}{r})$$,   where $$r$$ is the radius of earth.
    Thus $$g$$ is not constant throughout.
    Also  for  $$d=200  m$$                $$g'= g(1-\dfrac{200}{6400\times 1000})$$
    Now       $$\dfrac{g-g'}{g} \times 100= .003$$ %
    Thus $$g$$ is much more less than $$1$$%.
  • Question 2
    1 / -0
    The angular velocity of rotation of the earth in order to make the effective acceleration due to gravity equal to zero at equator should be $$g=10m/s^2, R=6400 km$$.
    Solution
    $$g'=g-\omega^2R cos^2\theta$$
    At equator $$g'=0$$
    $$cos\theta =0$$
    $$g=\omega^2R$$
    $$\omega^2=\frac {g}{R}$$
    $$\omega=\sqrt {\dfrac {g}{R}}=\sqrt {\dfrac {10}{6400\times 1000}}$$
    $$=\sqrt {\dfrac {1}{640000}}=\dfrac {1}{800}=1.25\times 10^{-3} rad/sec.$$
  • Question 3
    1 / -0
    The ratio of the radii of the planets $$P_{1}$$ and $$P_{2}$$ is $$k_{1}.$$ The corresponding ratio of the acceleration due to the gravity on them is $$k_{2}.$$ The ratio of the escape velocities from them will be
    Solution
    $$v_{e}=\sqrt{2gR}$$
    $$\therefore \dfrac{(v_{e})p_{1}}{(v_{e})p_{2}}=\dfrac{\sqrt{g_{1}R_{1}}}{\sqrt{g_{2}R_{2}}}=\sqrt{\left \{ \left ( \dfrac{g_{1}}{g_{2}} \right )\times \left ( \dfrac{R_{1}}{R^{2}} \right ) \right \}}=\sqrt{k_{1}k_{2}}$$
  • Question 4
    1 / -0
    A planet is revolving in an elliptical orbit around the sun as shown in figure.The areal velocity (area swapped by the radius vector with respect to sun in unit time) is :

    Solution
    Kepler's law of periods says that the area swept by a planet for a certain time interval is constant.
    i.e $$\dfrac {dA}{dt}=\dfrac {L}{2m}$$; where $$L$$ is the angular momentum and is constant.

    Therefore, $$\dfrac {dA}{dt}$$ is constant.
    $$\dfrac {dA}{dt}=\dfrac {L}{2m}=\dfrac {mv_2r_2}{2m}=\dfrac {1}{2}v_2r_2$$
  • Question 5
    1 / -0

    Directions For Questions

    The earth does not have a uniform density; it is most dense at its centre and least dense at its surface. An approximation of its density is  $$\rho (r) = (A - Br)$$, where $$A = 12,700 kg/m^3, B = 1.50 \times 10^{-3} kh/m^4$$ and  $$r$$  is the distance from the centre of earth. Use $$ R = 6.4 \times 10^6$$ m for the radius of earth approximated as a  sphere, Imagine dividing the earth into concentric, elementary spherical shells. Each shell has radius $$r$$,  thickness $$dr$$, volume  $$dV$$ and mass $$dm = \rho (r) dV$$. By integrating  $$dm$$  from zero to $$R$$  the mass of earth can be found. Knowing the fact that a uniform spherical shell gives no contribution to acceleration due to gravity inside it, we can also find  $$g$$  as a function of $$r$$.

    ...view full instructions

    Acceleration due to gravity as a function of $$r$$ is given by :
    Solution
    $$g = \dfrac {GM(r)}{r^2} = \dfrac {G.\dfrac{4}{3}\pi r^3 (A - \dfrac {3}{4}Br)}{r^2} = \dfrac {4 \pi Gr}{3} \left[A - \dfrac {3}{4} Br \right]$$
  • Question 6
    1 / -0
    A planet of radius $$R =1/10 \times {(radius \quad of \quad earth)}$$ has the same mass density as Earth. Scientist dig a well of depth $$\dfrac{R}{5}$$ on it and lower a wire of the same length and of linear mass density $$10^{-3} kgm^{-3}$$ into it. If the wire is not touching anywhere, the force applied at the top of the wire by a person holding it in places is (take the radius of earth $$ = 6\times 10^6$$ and the acceleration due to gravity on earth is $$10ms^{-2}$$)
    Solution
    $$R_e$$ is the radius of the earth
    $$g_e=\dfrac{GM_e}{R_e^2}=G\dfrac{4}{3}\pi R_e\rho$$
    Now g at the mentioned planet is given as
    $$g_p=\dfrac{GM}{r^2}$$, here $$m=\dfrac{4}{3}\pi r^3\rho$$
    Thus $$g_p=G\dfrac{4}{3}\pi r\rho$$
    Thus we get $$F=\displaystyle\int^R_{4R/5}\lambda g_p dr$$
    $$ F= \lambda \times G\dfrac{4}{3}\pi \rho\times \dfrac{9R^2}{50}$$
    Solving, we get 
    $$ F= 108N $$
  • Question 7
    1 / -0
    The ratio of the earth's orbital angular momentum (about the Sun) to its mass is $$4.4\times 10^{15} m^2s^{-1}$$. The area enclosed by the earth's orbit is approximately $$\underline{\hspace{0.5in}} m^2$$.
    Solution
    Areal velocity of a planet around the Sun is constant and is given by
    $$\dfrac {dA}{dt}=\dfrac {L}{2m}\Rightarrow dA=\dfrac {L}{2m}dt$$
    Integrating both sides $$\int dA=\dfrac {L}{2m}\int dt\Rightarrow A=\dfrac {L}{2m}\cdot T$$
    where $$L=$$ angular momentum of the planet (earth) about the Sun and $$m=$$ mass of planet (earth).
    Hence, $$A=\dfrac {L}{2m}T=\dfrac {1}{2}\times 4.4\times 10^{15}\times 365\times 24\times 3600 m^2$$
    $$Area=6.94\times 10^{22}m^2$$
  • Question 8
    1 / -0
    If the change in the value of $$g$$ at a height $$h$$ above the surface of the earth is the same as at a depth $$x$$ below it when both $$x$$ and $$h$$ are much smaller than the radius of the earth, then
    Solution
    $$\textbf{Hint}$$: Apply the formula of acceleration due to gravity above and below the earth surface.
    $$\textbf{Step 1}$$:
    We know acceleration due to gravity on the earth's surface is given by $$g=\dfrac{GM}{R^2}$$ where $$G$$ is gravitational constant, $$R$$ is the radius of the earth and $$M$$ is the mass of the earth.
    Given that the change in value of $$g$$ at a height $$h$$ above the surface of the earth is the same as at a depth $$x$$ below it.
    $$g \propto \dfrac{1}{R^2}$$
    $$g_h \propto \dfrac{1}{(R+h)^2}$$
    $$\dfrac{g_h}{g}=\dfrac{R^2}{(R+h)^2}$$
    $$ \implies \dfrac{g_h}{g}=\dfrac{1}{(1+\dfrac{h}{R})^2}$$
    $$\implies \dfrac{g_h}{g}=(1-\dfrac{2h}{R})$$
    $$\implies g_h=g- \dfrac{2gh}{R}$$
    $$ \implies g-g_h=\dfrac{2gh}{R}$$
    $$\textbf{Step 2}$$:
    The acceleration due to gravity at depth $$x$$ is given by
    $$g_x=\dfrac{4}{3}G_p(R-x)$$
    So, $$g_x \propto (R-x)$$
    $$\dfrac{g_x}{g}=\dfrac{R-x}{R}$$
    $$\dfrac{g_x}{g}=1-\dfrac{x}{R}$$
    $$g-g_x=\dfrac{gx}{R}$$
    Given that the change in value of $$g$$ at a height $$h$$ above the surface of the earth is the same as at a depth $$x$$ below it.
    $$g-g_h=g-g_x$$
    $$\dfrac{2gh}{R}=\dfrac{gx}{R}$$
    $$x=2h$$
    Thus option B is correct



  • Question 9
    1 / -0
    Calculate energy needed for moving a mass of $$4kg$$ from the centre of the earth to its surface (in joule). If radius of the earth is 6400 km and acceleration due to gravity at the surface of the earth is
    $$g = 10 m/sec^2$$
    Solution
    $$W = U_R - U_C =  [- \dfrac {GMm}{R} + \dfrac {3GMm}{2R}]$$
    $$\Rightarrow \dfrac {GMm}{2R} = \dfrac {mgR^2}{2R}$$

    $$\Rightarrow mgR/2 = 2gR = 2 \times 10 \times 6400 \times 10^3 = 1.28 \times 10^8 J$$
  • Question 10
    1 / -0
    The mass of the Jupiter is $$1.9\times 10^{27}\ kg$$ and that of the sun is $$1.99\times 10^{38}\ kg$$. The mean distance of the Jupiter from the sun is $$7.8\times 10^{11}\ m$$. Speed of the Jupiter is (assuming that Jupiter moves in a circular orbit around the sun)
    Solution
    $$F = \dfrac{GMm}{r^2}$$

    $$  = \dfrac{6.67\times 10^{-11}\times (1.99\times 10^{30})\times (1.9\times 10^{27})}{(7.8\times 10^{11})^2}$$

    $$  = 4.14\times 10^{23}  N$$

    Now let its speed of jupiter be $$v$$, then

    $$F = \dfrac{mv^2}{R}$$

    $$\Rightarrow  v = \sqrt{\dfrac{FR}{m}}$$

    $$  = \sqrt{\dfrac{(7.8\times 10^{11})\times (4.10\times 10^{23})}{(1.9\times 10^{27})}}$$

    $$  = 1.304\times 10^4 m/sec$$.
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