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ira [324]
3 years ago
14

A 2 nC point charge is at the origin, and a second 5 nC point charge is on the x-axis at x = 8 m. Find the electric field (magni

tude and direction) at the point x = 2 m.
Physics
1 answer:
dimaraw [331]3 years ago
7 0

Answer:

The magnitude of  the electric field is 5.75 N/C towards positive x- axis.

Explanation:

Given that,

Point charge at origin = 2 nC

Second charge = 5 nC

Distance at x axis = 8 m

We need to calculate the electric field at the point x = 2 m

Using formula of electric field

E=\dfrac{1}{4\pi\epsilon_{0}}(\dfrac{q_{1}}{r_{1}^2}+\dfrac{q_{2}}{r_{2}^2})

Put the value into the formula

E=9\times10^{9}\times(\dfrac{2\times10^{-9}}{2^2}+\dfrac{5\times10^{-9}}{(8-2)^2})

E=5.75\ N/C

The direction is toward positive x- axis.

Hence, The magnitude of  the electric field is 5.75 N/C towards positive x- axis.

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A mass on a spring oscillates with a period T. Part A If both the mass and the force constant of the spring are doubled, the new
garik1379 [7]

Answer:

The new time period will be T.

Explanation:

The time period in terms of spring constant and mass is given by :

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4 0
3 years ago
A high-temperature, gas-cooled nuclear reactor consists of a composite, cylindrical wall for which a thorium fuel element (kth =
WARRIOR [948]

Answer:

a) T_1 = 938 K , T_2 = 931 K

b) To prevent softening of the materials, which would occur below their  melting points, the reactor should not be operated much above:

                                      q = 3*10^8 W/m^3

Explanation:

Given:

- See the attachment for the figure for this question.

- Melting point of Thorium T_th = 2000 K

- Melting point of Thorium T_g = 2300 K

Find:

a) If the thermal energy is uniformly generated in the fuel element at a rate q = 10^8 W/m^3 then what are the temperatures T_1 and T_2 at the inner and outer surfaces, respectively, of the fuel element?

b) Compute and plot the temperature distribution in the composite wall for selected values of q.  What is the maximum allowable value of q.

Solution:

part a)

- The outer surface temperature of the fuel, T_2, may be determined from the rate equation:

                                 q*A_th = T_2 - T_inf / R'_total

Where,

           A_th: Area of the thorium section

           T_inf: The temperature of coolant = 600 K

           R'_total: The resistance per unit length.

- Calculate the resistance per unit length R' from thorium surface to coolant:

           R'_total = Ln(r_3/r_2) / 2*pi*k_g + 1 / 2*pi*r_3*h

Plug in values:

           R'_total = Ln(14/11) / 2*pi*3 + 1 / 2*pi*0.014*2000

           R'_total = 0.0185 mK / W

- And the heat rate per unit length may be determined by applying an energy balance to a control surface  about the fuel element. Since the interior surface of the element is essentially adiabatic, it follows that:

           q' = q*A_th = q*pi*(r_2^2 - r_1^2)

           q' = 10^8*pi*(0.011^2 - 0.008^2) = 17,907 W / m

Hence,

           T_2 = q' * R'_total + T_inf

           T_2 = 17,907*0.0185 + 600

          T_2 = 931 K

- With zero heat flux at the inner surface of the fuel element, We will apply the derived results for boundary conditions as follows:

 T_1 = T_2 + (q*r_2^2/4*k_th)*( 1 - (r_1/r_2)^2) - (q*r_1^2/2*k_th)*Ln(r_2/r_1)

Plug values in:

 T_1 = 931+(10^8*0.011^2/4*57)*( 1 - (.8/1.1)^2) - (10^8*0.008^2/2*57)*Ln(1.1/.8)

 T_1 = 931 + 25 - 18 = 938 K

part b)

The temperature distributions may be obtained by using the IHT model for one-dimensional, steady state conduction in a hollow tube. For the fuel element (q > 0),  an adiabatic surface condition is  prescribed at r_1 while heat transfer from the outer surface at r_2 to the coolant is governed by the thermal  resistance:

                              R"_total = 2*pi*r_2*R'_total

                              R"_total = 2*pi*0.011*0.0185 = 0.00128 m^2K/W

- For the graphite ( q = 0 ), the value of T_2 obtained from the foregoing solution is prescribed as an inner boundary condition at r_2, while a convection condition is prescribed at the outer surface (r_3).

- For 5*10^8 < q and q > 5*10^8, the distributions are given in attachment.

The graphs obtained:

- The comparatively large value of k_t yields small temperature variations across the fuel element,  while the small value of k_g results in large temperature variations across the graphite.

Operation  at q = 5*10^8 W/^3  is clearly unacceptable, since the melting points of thorium and graphite are exceeded  and approached, respectively. To prevent softening of the materials, which would occur below their  melting points, the reactor should not be operated much above:

                                      q = 3*10^8 W/m^3

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3 years ago
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Answer:

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