Calculate the ratio of the voltage in the secondary coil to the voltage in the primary coil, Vprimary ​Vsecondary ​​, for a step up transformer if the no of turns in the primary coil is Nprimary ​=10 and the no of turns in the secondary coil is Nsecondary ​=12,903. Nsecondary ​Nprimary ​​=Vsecondary ​Vprimary ​​

For oil flow through a pipe, velocity increases with increase in area of cross section. Option 3 is correct.

To determine the head loss due to friction in a pipe, we can use the Darcy-Weisbach equation:

ΔP = λ * (L/D) * (ρ * V² / 2)

Where:

ΔP is the pressure drop (given as 9.81 kPa)

λ is the friction factor

L is the length of the pipe

D is the diameter of the pipe

ρ is the density of the fluid (water in this case)

V is the velocity of the fluid

We can rearrange the equation to solve for the head loss (H):

H = (ΔP * 2) / (ρ * g)

Where g is the acceleration due to gravity (9.81 m/s²).

Given the pressure drop (ΔP) of 9.81 kPa, we can calculate the head loss due to friction.

H = (9.81 kPa * 2) / (ρ * g)

Now, let's address the second part of your question regarding oil flow through a pipe and how velocity changes with respect to pressure and cross-sectional area.

With an increase in pressure at a cross section: When the pressure at a cross section increases, it typically results in a decrease in velocity due to the increased resistance against flow.

With a decrease in area of the cross section: According to the principle of continuity, when the cross-sectional area decreases, the velocity of the fluid increases to maintain the same flow rate.

With an increase in area of the cross section: When the cross-sectional area increases, the velocity of the fluid decreases to maintain the same flow rate.

The velocity does not depend solely on the area of the cross section. It is influenced by various factors such as pressure, flow rate, and pipe properties.

Therefore, the correct answer to the question is option 4: The velocity does not depend on the area of the cross section alone.

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The resistance of the 110 W bulb is 131 Ω.

The formula to calculate resistance is [tex]R = V^2 / P[/tex] where R is resistance, V is voltage, and P is power.

R = V^2 / P, where V[tex]= V_max / √2[/tex]  where V_max is the maximum voltage.

The maximum voltage is 170 V.

Therefore,

V = V_max / √2

= 170 / √2

= 120 V.

R = V^2 / P

= (120)^2 / 45

= 320 Ω

Therefore, the resistance of the light bulb is 320 Ω.

(b) Similarly, R = V^2 / P,

where V = V_max / √2.V_max

= 170 V, and

P = 110 W.

Therefore,

V = V_max / √2

= 170 / √2 = 120 V.

R = V^2 / P

= (120)^2 / 110

= 131 Ω

Therefore, the resistance of the 110 W bulb is 131 Ω.

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According to the question (a). The mass of the water displaced by the boat is 6700 kg. (b). The weight of the boat is 65560 N.

a. To calculate the mass of the water displaced by the boat, we can use the formula:

[tex]\[ \text{mass} = \text{volume} \times \text{density} \][/tex]

Given that the volume of water displaced is 6.7 m³ and the density of water is 1000 kg/m³, we can substitute these values into the formula:

[tex]\[ \text{mass} = 6.7 \, \text{m³} \times 1000 \, \text{kg/m³} \][/tex]

[tex]\[ \text{mass} = 6700 \, \text{kg} \][/tex]

Therefore, the mass of the water displaced by the boat is 6700 kg.

b. To calculate the weight of the boat, we need to know the gravitational acceleration in the specific location. Assuming the standard gravitational acceleration of approximately 9.8 m/s²:

[tex]\[ \text{weight} = \text{mass} \times \text{acceleration due to gravity} \][/tex]

Given that the mass of the water displaced by the boat is 6700 kg, we can substitute this value into the formula:

[tex]\[ \text{weight} = 6700 \, \text{kg} \times 9.8 \, \text{m/s}^2 \][/tex]

[tex]\[ \text{weight} = 65560 \, \text{N} \][/tex]

Therefore, the weight of the boat is 65560 N.

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The decay of radioactive atoms is an exponential process, and the amount of a radioactive substance remaining after time t can be modeled by the equation:

N(t) = N0 * e^(-λt)

where N0 is the initial amount of the substance, λ is the decay constant, and e is the base of the natural logarithm. The half-life of Rn-222 is given as 3.823 days, which means that the decay constant is:

λ = ln(2)/t_half = ln(2)/3.823 days ≈ 0.1814/day

Let N(t) be the amount of Rn-222 at time t (measured in days) after the initial measurement, and let N0 = 30 g be the initial amount. We want to find the time t such that N(t) = 7.5 g.

Substituting the given values into the equation above, we get:

N(t) = 30 * e^(-0.1814t) = 7.5

Dividing both sides by 30, we get:

e^(-0.1814t) = 0.25

Taking the natural logarithm of both sides, we get:

-0.1814t = ln(0.25) = -1.3863

Solving for t, we get:

t = 7.64 days

Therefore, it will take approximately 7.64 days for 30 grams of Rn-222 to decay to 7.5 grams.

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The wavelength of this wave with the linear mass density, and wave function provided for is calculated to be 0.21 meters.

To find the wavelength of the wave represented by the given wave function, we can start by identifying the wave equation:

y(x, t) = A sin(kx - ωt)

In this equation, A represents the amplitude of the wave, k is the wave number (related to the wavelength), x is the position along the string, ω is the angular frequency, and t is time.

Comparing the given wave function y(x, t) = 0.4 sin(kx - 12rtt) to the wave equation, we can determine the following:

Amplitude (A) = 0.4

Wave number (k) = ?

Angular frequency (ω) = 12rt

The power associated with the wave is also given as 34.11 W. The power of a wave can be calculated using the formula:

Power = (1/2)uω^2A^2

Substituting the given values into the power equation:

The correct calculation is:

(1/2) * (0.05) * (0.4)^2 = 0.04

Now, let's continue with the calculation:

Power = 34.11 W

Power = (1/2) * (0.05) * (0.4)^2

0.04 = 34.11

(12rt)^2 = 34.11 / 0.04

(12rt)^2 = 852.75

12rt = sqrt(852.75)

12rt ≈ 29.20188

Now, we can calculate the wavelength (λ) using the wave number (k):

λ = 2π / k

λ = 2π / (12rt)

λ = 2π / 29.20188

λ ≈ 0.21 m

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The height difference between the lowest and highest point of the roof is needed. By using the trigonometric function tangent, we can determine the height difference between the lowest and highest point of the gable-shaped roof.

To calculate the height difference between the lowest and highest point of the roof, we can use trigonometry. Here's how:

1. Identify the given information: The width of the building is 10 m, and the roof is angled at 23.0° from the horizontal.

2. Draw a diagram: Sketch a triangle representing the gable roof. Label the horizontal base as the width of the building (10 m) and the angle between the base and the roof as 23.0°.

3. Determine the height difference: The height difference corresponds to the vertical side of the triangle. We can calculate it using the trigonometric function tangent (tan).

  tan(angle) = opposite/adjacent

  In this case, the opposite side is the height difference (h), and the adjacent side is the width of the building (10 m).

  tan(23.0°) = h/10

  Rearrange the equation to solve for h:

  h = 10 * tan(23.0°)

  Use a calculator to find the value of tan(23.0°) and calculate the height difference.

By using the trigonometric function tangent, we can determine the height difference between the lowest and highest point of the gable-shaped roof. The calculated value will provide the desired information about the vertical span of the roof.

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The fraction of initial energy lost in this collision is 0. This implies that no energy is lost, indicating an elastic collision.

To determine the fraction of initial energy lost in the collision, we need to compare the initial kinetic energy with the final kinetic energy after the collision.

Given:

Initial speed of the first stone (v_1) = 2.0 m/s

Angle of deflection for the first stone (θ_1) = 28°

Angle of deflection for the second stone (θ_2) = 42°

Let's calculate the final speeds of the first and second stones using the given information:

Using trigonometry, we can find the components of the final velocities in the x and y directions for both stones.

For the first stone:

vx_1 = v_1 * cos(θ_1)

vy_1 = v_1 * sin(θ_1)

For the second stone:

vx_2 = v_2 * cos(θ_2)

vy_2 = v_2 * sin(θ_2)

Since the second stone is initially stationary, its initial velocity is zero (v_2 = 0).

Now, we can calculate the final velocities:

vx_1 = v1 * cos(θ_1)

vy_1 = v1 * sin(θ_1)

vx_2 = 0 (as v_2 = 0)

vy_2 = 0 (as v_2 = 0)

The final kinetic energy (Kf) can be calculated using the formula:

Kf = (1/2) * m * (vx1^2 + vy1^2) + (1/2) * m * (vx2^2 + vy2^2)

Since the second stone is initially stationary, its final kinetic energy is zero:

Kf = (1/2) * m * (vx_1^2 + vy_1^2)

The initial kinetic energy (Ki) can be calculated using the formula:

Ki = (1/2) * m * v_1^2

Now, we can determine the fraction of initial energy lost in the collision:

Fraction of initial energy lost = (K_i - K_f) / K_i

Substituting the expressions for K_i and K_f:

[tex]Fraction of initial energy lost = [(1/2) * m * v1^2 - (1/2) * m * (vx_1^2 + vy_1^2)] / [(1/2) * m * v_1^2]Simplifying and canceling out the mass (m):Fraction of initial energy lost = (v_1^2 - vx_1^2 - vy_1^2) / v_1^2Using the trigonometric identities sin^2(θ) + cos^2(θ) = 1, we can simplify further:[/tex]

Therefore, the fraction of initial energy lost in this collision is 0. This implies that no energy is lost, indicating an elastic collision.

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#SPJ11[tex]Fraction of initial energy lost = (v_1^2 - vx_1^2 - vy_1^2) / v_1^2Fraction of initial energy lost = (v_1^2 - v_1^2 * cos^2(θ_1) - v_1^2 * sin^2(θ_1)) / v_1^2Fraction of initial energy lost = (v_1^2 * (1 - cos^2(θ_1) - sin^2(θ_1))) / v_1^2Fraction of initial energy lost = (v_1^2 * (1 - 1)) / v1^2Fraction of initial energy lost = 0[/tex]

Given that at a depth of 5.00 km, the force per unit area is 5.00×10^7 N/m², we can calculate the pressure at that depth.

In Example 5.6 of the mentioned chapter, we are asked to calculate the fractional decrease in volume of seawater at a certain depth. The depth is given as W meters, and we need to find the force per unit area and solve the example accordingly.

Pressure (P) is defined as force per unit area, so we have:

P = 5.00×10^7 N/m²

To express the pressure in atmospheres, we can use the conversion factor:

1 atm = 1.013×10^5 N/m²

Therefore, the pressure at 5.00 km depth is:

P = (5.00×10^7 N/m²) × (1 atm / 1.013×10^5 N/m²) ≈ 4.93×10² atm

Now, we can proceed to calculate the fractional decrease in volume (Δ₀) using the equation Δ = V/V₀ - 1, where Δ represents the fractional change in volume and V₀ is the initial volume.

Solving the equation for V, we find:

Δ = V/V₀ - 1 = 10⁻⁶

Simplifying, we get:

V/V₀ - 1 = 10⁻⁶

V/V₀ = 1 + 10⁻⁶

V/V₀ ≈ 1.000001

Therefore, Δ₀ = V/V₀ - 1 - 1 ≈ -6.00×10⁻⁶.

Since pressure is usually expressed in atmospheres, we can rewrite the result as:

Δ₀ ≈ -2.96×10⁻³ atm⁻¹.

The negative sign indicates that as the pressure increases, the volume decreases. Hence, the fractional decrease in volume of seawater at the given depth is approximately -2.96×10⁻³ atm⁻¹.

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The ratio of the radius ry of particle 1's path to the radius rz of particle 2's path is 6:5.

In this scenario, both particle 1 and particle 2 have the same kinetic energy and are moving perpendicular to a uniform magnetic field B. The motion of charged particles in a magnetic field is determined by the equation qvB = mv²/r, where q is the charge, v is the velocity, B is the magnetic field, m is the mass, and r is the radius of the path.

Since both particles have the same kinetic energy, their velocities are equal. Using the equation mentioned above, we can equate the expressions for the radii of the paths of particle 1 and particle 2. Solving for the ratio of the radii, we find that ry/rz = (m1/m2)^(1/2), where m1 and m2 are the masses of particle 1 and particle 2, respectively. Plugging in the given masses, we get ry/rz = (6.0/5.0)^(1/2) = 6/5. Therefore, the ratio of the radius ry of particle 1's path to the radius rz of particle 2's path is 6:5.

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The correct answer is option c. 51°. The critical angle between glass and water can be determined based on their refractive indices. In this scenario, where the refractive index of glass is 1.8 and the refractive index of water is 1.4, the critical angle can be calculated.

To find the critical angle, we can use the formula: critical angle = sin^(-1)(n2/n1), where n1 is the refractive index of the first medium (glass) and n2 is the refractive index of the second medium (water). Plugging in the values, the critical angle can be calculated as sin^(-1)(1.4/1.8). Evaluating this expression, we find that the critical angle between glass and water is approximately 51°.

Therefore, the correct answer is option c. 51°. This critical angle signifies the angle of incidence beyond which light traveling from glass to water will undergo total internal reflection.

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Given:

Frequency, f = 107.3 MHz

Intensity, I = 0.225 W/m²

Power = 6 MW

The impedance of the medium in free space, ρ = 377 Ohms

a) We can apply the inverse square law to calculate wave strength as the square of the distance from the radio station. The square of the distance from the source has an inverse relationship with the intensity.

According to the inverse square law:

I₂ = I₁ × (d₁ / (2d₁))²

Simplifying the equation:

I₂ = I₁ × (1/4)

I₂ = 0.225 W/m² × (1/4)

I₂ = 0.056 W/m²

Hence, the intensity of the wave, twice the distance from the radio station, is 0.056 W/m².

b) The wavelength of the transmitted signal  is:

λ = c / f

λ = (3 × 10⁸ m/s) / (107.3 × 10⁶Hz)

λ = 0.861 mm

Hence, the wavelength of the transmitted signal is 0.861 mm.

c) To find the distance from the source where the intensity of the wave is 0.113 W/m². From the inverse law relation:

I = 1 ÷ √d₂

d₂ = 1 ÷ √ 0.113)

d₂ = 2.94 m

Hence, the distance is 2.94 m.

d) The absorption pressure exerted by the wave is:

P = √(2 ×   I ×  ρ)

Here, (P) is the absorption pressure, (I) is the intensity, and (ρ) is the impedance of the medium.

Substituting the values:

P = √(2  × 0.113 ×  377 )

P = 0.38 × 10⁻⁹ N/m²

Hence, the absorption pressure exerted by the wave at the given distance is  0.38 × 10⁻⁹ N/m² .

e) The effective electric field (rms) exerted by the wave is:

E = √(2 × Z ×  I)

Here,  E is the effective electric field, Z is the impedance of the medium, and I is the intensity.

Substituting the values:

E = √(2 ×  377 ohms ×  0.113 W/m²)

E = 9.225 V/m

The rms electric field is:

E₁ = E÷ 1.4

E₁ = 9.225 ÷ 1.4

E₁ = 6.52 V/m

Hence, the effective electric field (rms) exerted by the wave at the given distance is 6.52 V/m.

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The expression for the image distance, d is;d' = 0.00093 m

Given that: Height of candle, h = 0.24 m

Distance of candle from the left of the lens, d= 0.48 m

Focal length of the diverging lens, f = -0.071 m

Image distance, d' is given by the lens formula as;1/f = 1/d - 1/d'

Taking the absolute magnitude of f, we have f = 0.071 m

Substituting the values in the above equation, we have; 1/0.071 = 1/0.48 - 1/d'14.0845

= (0.048 - d')/d'

Simplifying the equation above by cross multiplying, we have;

14.0845d' = 0.048d' - 0.048d' + 0.071 * 0.48d'

= 0.013125d'

= 0.013125/14.0845

= 0.00093 m (correct to 3 significant figures).

Therefore, the expression for the image distance, d is;d' = 0.00093 m

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The charge on the sphere is approximately 1.68 × 10^-7 C.

We can use the formula for the electric field strength near the surface of a charged sphere to solve this problem. The electric field strength near the surface of a charged sphere is given by:

E = (1 / 4πε₀) * (Q / r^2)

where E is the electric field strength, Q is the charge on the sphere, r is the distance from the center of the sphere, and ε₀ is the permittivity of free space.

In this problem, we are given the electric field strength E and the distance from the surface of the sphere r. We can use these values to solve for the charge Q.

First, we need to find the radius of the sphere. The diameter of the sphere is given as 12 cm, so the radius is:

r = d/2 = 6 cm

Substituting the given values, we get:

100 kN/C = (1 / 4πε₀) * (Q / (0.03 m)^2)

Solving for Q, we get:

Q = 4πε₀ * r^2 * E

where ε₀ is the permittivity of free space, which has a value of 8.85 × 10^-12 C^2/(N·m^2).

Substituting the given values, we get:

Q = 4π * 8.85 × 10^{-12} C^2/(N·m^2) * (0.06 m)^2 * 100 kN/C

Solving for Q, we get:

Q ≈ 1.68 × 10^{-7} C

Therefore, the charge on the sphere is approximately 1.68 × 10^{-7} C.

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Explanation:

D. A Step Down Transformer is used to decrease the voltage.

A transformer is a device that is used to transfer electrical energy from one circuit to another by electromagnetic induction. A step-down transformer is a type of transformer that is designed to reduce the voltage from the input to the output.

In a step-down transformer, the number of turns in the secondary coil is less than the number of turns in the primary coil. As a result, the voltage in the secondary coil is lower than the voltage in the primary coil.

Step-down transformers are commonly used in power distribution systems to reduce the high voltage in power lines to a lower, safer voltage level for use in homes and businesses. They are also used in electronic devices to convert high voltage AC power to low voltage AC power, which is then rectified to DC power.

The de Broglie wavelength of the electron after the photon has been scattered is approximately -1.12 picometers (-1.12 pm).

To determine the de Broglie wavelength of the electron after the photon scattering, we can use the conservation of momentum and energy.

Given:

Wavelength of the photon before scattering (λ_initial) = 1.73 pm

Scattering angle (θ) = 147°

The de Broglie wavelength of a particle is given by the formula:

λ = h / p

where λ is the de Broglie wavelength, h is the Planck's constant, and p is the momentum of the particle.

Before scattering, both the photon and the electron have momentum. After scattering, the momentum of the electron changes due to the transfer of momentum from the photon.

We can use the conservation of momentum to relate the initial and final momenta:

p_initial_photon = p_final_photon + p_final_electron

Since the photon is initially stationary, its initial momentum (p_initial_photon) is zero. Therefore:

p_final_photon + p_final_electron = 0

p_final_electron = -p_final_photon

Now, let's calculate the final momentum of the photon:

p_final_photon = h / λ_final_photon

To find the final wavelength of the photon, we can use the scattering angle and the initial and final wavelengths:

λ_final_photon = λ_initial / (2sin(θ/2))

Substituting the given values:

λ_final_photon = 1.73 pm / (2sin(147°/2))

Using the sine function on a calculator:

sin(147°/2) ≈ 0.773

λ_final_photon = 1.73 pm / (2 * 0.773)

Calculating the value:

λ_final_photon ≈ 1.73 pm / 1.546 ≈ 1.120 pm

Now we can calculate the final momentum of the photon:

p_final_photon = h / λ_final_photon

Substituting the value of Planck's constant (h) = 6.626 x 10^-34 J·s and converting the wavelength to meters:

λ_final_photon = 1.120 pm = 1.120 x 10^-12 m

p_final_photon = (6.626 x 10^-34 J·s) / (1.120 x 10^-12 m)

Calculating the value:

p_final_photon ≈ 5.91 x 10^-22 kg·m/s

Finally, we can find the de Broglie wavelength of the electron after scattering using the relation:

λ_final_electron = h / p_final_electron

Since p_final_electron = -p_final_photon, we have:

λ_final_electron = h / (-p_final_photon)

Substituting the values:

λ_final_electron = (6.626 x 10^-34 J·s) / (-5.91 x 10^-22 kg·m/s)

Calculating the value:

λ_final_electron ≈ -1.12 x 10^-12 m

Therefore, the de Broglie wavelength of the electron after the photon has been scattered is approximately -1.12 picometers (-1.12 pm).

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The energy consumption of the school building in a month is 277,703 kWh, and its carbon dioxide emissions are 85,994 kg.CO₂.

The calculation of energy consumption is derived from the formula given below:

Energy consumption = Energy load * Hours of use in a month / system efficiency

Energy load is equal to the product of building’s design heat loss coefficient and the degree day factor. Degree day factor is equal to the difference between the outdoor temperature and internal set point temperature, multiplied by the duration of that period, and summed over the entire month.

The carbon dioxide emissions for that month is calculated by multiplying the energy consumption by 0.31 kg.CO₂/kWh of gas.

As per the given data, energy load = 0.025MW/K * (20°C-5°C) * (24h-5.1h) * 30 days = 10,440 MWh, and the degree day factor is 15°C * (24h-5.1h) * 30 days = 10,818°C-day.

Therefore, the energy consumption of the school building in a month is 277,703 kWh, and its carbon dioxide emissions are 85,994 kg.CO₂.

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The electric-field between the plates of the capacitor is approximately 2831.46 V/m.

The electric field between the plates of a capacitor can be determined by using the formula: Electric field (E) = Voltage difference (V) / Plate separation distance (d)

In this case, we are given the following values:

Charge (Q) = 14.35 microC = 14.35 * 10^-6 C

Voltage difference (V) = 37.25 V

Plate separation distance (d) = 13.16 mm = 13.16 * 10^-3 m

We can calculate the electric field as follows:

E = V / d

E = 37.25 V / (13.16 * 10^-3 m)

E = 2831.46 V/m

Therefore, the electric-field between the plates of the capacitor is approximately 2831.46 V/m.

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The focal length of the convex mirror is -2 m. The negative sign indicates that the mirror has a diverging effect, as is characteristic of convex mirrors.

To determine the focal length of a convex mirror, we can use the mirror equation:

1/f = 1/d_o + 1/d_i

Where f is the focal length, d_o is the object distance (distance of the object from the mirror), and d_i is the image distance (distance of the image from the mirror).

In this case, the object distance (d_o) is given as 2 m, and the image distance (d_i) is given as -1 m (since the image is formed behind the mirror, the distance is negative).

Substituting the values into the mirror equation:

1/f = 1/2 + 1/-1

Simplifying the equation:

1/f = 1/2 - 1/1

1/f = -1/2

To find the value of f, we can take the reciprocal of both sides of the equation:

f = -2/1

f = -2 m

Therefore, the focal length of the convex mirror is -2 m. The negative sign indicates that the mirror has a diverging effect, as is characteristic of convex mirrors.

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The accuracy of the given timer is 0.346 s.The accuracy of the ruler is not provided in the given information. The relative error in measured acceleration due to gravity (g) in cm is not specified in the question. If the ball falls from a height of y = 100.0 cm or y = 60.0 cm, the value of g (gravitational acceleration) will remain constant.

The equation provided, 2y = [tex]gt^2[/tex], relates the distance fallen (y) to the time squared [tex](t^2)[/tex], but it does not depend on the initial height.

The gravitational acceleration, g, is constant near the surface of the Earth regardless of the starting height of the object.

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The fraction of the ice above the water level is 0.6 meters (option c).

The ice floats on water because its density is less than that of water. The volume of ice seen above the surface is dependent on its density, which is less than water density. The volume of the ice is dependent on the water that it displaces. An ice cube measuring 1 m has a volume of 1m^3.

Let V be the fraction of the volume of ice above the water, and let the volume of the ice be 1m^3. Therefore, the volume of water displaced by ice will be V x 1m^3.The mass of the ice is 917kg/m^3 * 1m^3, which is equal to 917 kg. The mass of water displaced by the ice is equal to the mass of the ice, which is 917 kg.The weight of the ice is equal to its mass multiplied by the gravitational acceleration constant (g) which is equal to 9.8 m/s^2.

Hence the weight of the ice is 917kg/m^3 * 1m^3 * 9.8m/s^2 = 8986.6N.The buoyant force of water will support the weight of the ice that is above the surface, hence it will be equal to the weight of the ice above the surface. Therefore, the buoyant force on the ice is 8986.6 N.The formula for the buoyant force is as follows:

Buoyant force = Volume of the fluid displaced by the object × Density of the fluid × Gravity.

Buoyant force = V*1m^3*1025 kg/m^3*9.8m/s^2 = 10002.5*V N.

As stated earlier, the buoyant force is equal to the weight of the ice that is above the surface. Hence, 10002.5*V N = 8986.6

N.V = 8986.6/10002.5V = 0.8985 meters.

To find the fraction of the volume of ice above the water, we must subtract the 0.4 m of ice above the water from the total volume of the ice above and below the water.V = 1 - (0.4/1)V = 0.6 meters.

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a) The entropy of mixing per one mole of formed air, is approximately 6.11 J/K. b) A specific value for the entropy of mixing per one mole of formed air cannot be determined

We find that the entropy of mixing per one mole of formed air is approximately 6.11 J/K. When gases are mixed together, the entropy of the system increases due to the increase in disorder. To calculate the entropy of mixing, we can use the formula:

ΔS_mix = -R * (x1 * ln(x1) + x2 * ln(x2))

where ΔS_mix is the entropy of mixing, R is the gas constant, x1 and x2 are the mole fractions of the individual gases, and ln is the natural logarithm. Since four moles of nitrogen and one mole of oxygen are mixed together to form air, the mole fractions of nitrogen and oxygen are 0.8 and 0.2, respectively. Substituting these values into the formula, along with the gas constant, we find ΔS_mix ≈ 6.11 J/K.

b) The entropy of mixing per one mole of formed air, when four moles of nitrogen and one mole of oxygen are mixed together at different temperatures, depends on the temperature difference between the gases.

The entropy change is given by ΔS_mix = R * ln(Vf/Vi), where Vf and Vi are the final and initial volumes, respectively. Since the temperatures are different, the final volume of the mixture will depend on the specific conditions. Therefore, a specific value for the entropy of mixing per one mole of formed air cannot be determined without additional information about the final temperature and volume.

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The mean free path of a photon in the core in mm can be calculated using the given information which are:Radius of solar core = 0.1R, where R is the solar radius.

The core contains 25% of the sun's total mass First, we will calculate the radius of the core:Radius of core, r = 0.1RWe know that the mass of the core, M = 0.25Ms, where Ms is the total mass of the sun.A formula that can be used to calculate the mean free path of a photon is given by:l = 1 / [σn]Where l is the mean free path, σ is the cross-sectional area for interaction and n is the number density of the target atoms/molecules.

Let's break the formula down for easier understanding:σ = πr² where r is the radius of the core n = N / V where N is the number of target atoms/molecules in the core and V is the volume of the core.l = 1 / [σn] = 1 / [πr²n]We can calculate N and V using the mass of the core, M and the mass of a single atom, m.N = M / m Molar mass of the sun.

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F_gravity = m1 * g,  F_normal = m1 * g * cos(θ), F_friction = μ * F_normal and  F_parallel = m1 * g * sin(θ).

Mass 1 experiences a downward gravitational force and an upward normal force from the ramp. It also experiences a kinetic friction force opposing its motion. Mass 2 experiences only a downward gravitational force.

Let's start by analyzing the forces acting on Mass 1. The gravitational force acting downward is given by the formula F_gravity = m1 * g, where m1 is the mass of Mass 1 (19 kg) and g is the acceleration due to gravity (approximately 9.8 m/s²).

The normal force, which is perpendicular to the ramp, counteracts a component of the gravitational force and can be calculated as F_normal = m1 * g * cos(θ), where θ is the angle of the ramp (50°).

The friction force opposing the motion of Mass 1 is given by the formula F_friction = μ * F_normal, where μ is the coefficient of kinetic friction (0.35) and F_normal is the normal force. Along the ramp, there is a component of the gravitational force acting parallel to the surface, which can be calculated as F_parallel = m1 * g * sin(θ).

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At point D, the resultant internal loadings in the beam consist of a shear force of 15 kN and a bending moment of 40 kNm in the clockwise direction. At point E, just to the right of the 15-kN load, the resultant internal loadings in the beam consist of a shear force of 40 kN and a bending moment of 80 kNm in the clockwise direction.

To determine the internal loadings in the beam at points D and E, we need to analyze the forces and moments acting on the beam.

At point D, which is located 2 m from the left end of the beam, there is a concentrated load of 15 kN acting downward. This load creates a shear force of 15 kN at point D. Additionally, there is a distributed load of 25 kN/m acting downward over a 1.5 m length of the beam from point C to D. To calculate the bending moment at D, we can use the equation:

M = -wx²/2

where w is the distributed load and x is the distance from the left end of the beam. Substituting the values, we have:

M = -(25 kN/m)(1.5 m)²/2 = -56.25 kNm

Therefore, at point D, the resultant internal loadings in the beam consist of a shear force of 15 kN (acting downward) and a bending moment of 56.25 kNm (clockwise).

Moving to point E, just to the right of the 15-kN load, we need to consider the additional effects caused by this load. The 15-kN load creates a shear force of 15 kN (acting upward) at point E, which is balanced by the 25 kN/m distributed load acting downward. As a result, the net shear force at point E is 25 kN (acting downward). The distributed load also contributes to the bending moment at point E, calculated using the same equation:

M = -wx²/2

Considering the distributed load over the 2 m length from point B to E, we have:

M = -(25 kN/m)(2 m)²/2 = -100 kNm

Adding the bending moment caused by the 15-kN load at point E (clockwise) gives us a total bending moment of -100 kNm + 15 kN x 2 m = -70 kNm (clockwise).

Therefore, at point E, the resultant internal loadings in the beam consist of a shear force of 25 kN (acting downward) and a bending moment of 70 kNm (clockwise).

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The work required to bring a +5.0 µC point charge from infinity to a point 2.0 m away from a +25 µC charge is 6.38 × 10^-5 joules.

To calculate the work, we can use the equation: Work = q1 * q2 / (4πε₀ * r), where q1 and q2 are the charges, ε₀ is the permittivity of free space, and r is the distance between the charges. Plugging in the given values, we get Work = (5.0 µC * 25 µC) / (4πε₀ * 2.0 m). Evaluating the expression, we find the work to be 6.38 × 10^-5 joules.Therefore, the work required to bring the +5.0 µC point charge from infinity to a point 2.0 m away from the +25 µC charge is 6.38 × 10^-5 joules.

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The magnitude of the magnetic force per unit length between the two wires is given by E = a × 10-N/m & the value of 'a' from the calculation we can get is 8.

To determine the value of 'a' in the expression E = a × 10-N/m x /m, we need to calculate the magnitude of the magnetic force per unit length between the two parallel wires when the current in each wire is I = 4 amps and the distance between the wires is L = 1 meter.

The magnetic force per unit length between two parallel wires carrying current can be calculated using the formula:

E = (μ₀ * I₁ * I₂) / (2πd)

where μ₀ is the permeability of free space (μ₀ ≈ [tex]4 \pi * 10^{-7[/tex] T·m/A), I₁ and I₂ are the currents in the wires, and d is the distance between the wires.

Plugging in the given values:

E = ([tex]4 \pi * 10^{-7[/tex]T·m/A * 4 A * 4 A) / (2π * 1 m)

E = ([tex]16 \pi * 10^{-7[/tex]T·m/A²) / (2π * 1 m)

E = [tex]8 * 10^{-7[/tex] T/m

Comparing this with the given expression E = a * 10-N/m x /m, we can see that 'a' must be equal to 8 to match the calculated value of E.

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The amount of current in an electrical device with a voltage source of Z volts that delivers 6.3 watts of electrical power is given by I = 6.3/Z.

Explanation:

Consider an electrical device connected to a voltage source of Z volts.

The device is designed to consume 6.3 watts of electrical power.

Calculate the amount of current flowing through the device.

Sketch:

+---------[Device]---------+

| |

----|--------Z volts--------|----

To calculate the current flowing through the electrical device, we can use the formula:

    Power (P) = Voltage (V) × Current (I).

Given that the power consumed by the device is 6.3 watts, we can express it as P = 6.3 W.

The voltage provided by the source is Z volts, so V = Z V.

We can rearrange the formula to solve for the current:

     I = P / V

Now, substitute the given values:

     I = 6.3 W / Z V

Therefore, the current flowing through the electrical device connected to a Z-volt source is 6.3 watts divided by Z volts.

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The amount of current flowing through the electrical device is 6.3 watts divided by the voltage source in volts (Z).

To calculate the current flowing through the electrical device, we can use the formula:

Power (P) = Voltage (V) × Current (I)

Given that the power (P) is 6.3 watts, we can substitute this value into the formula. The voltage (V) is represented as Z volts.

Therefore, we have:

6.3 watts = Z volts × Current (I)

Now, let's solve for the current (I):

I = 6.3 watts / Z volts

The sketch below illustrates the circuit setup:

  +---------+

  |         |

---|         |---

|  |         |  |

|  | Device  |  |

|  |         |  |

---|         |---

  |         |

  +---------+

    Voltage

    Source (Z volts)

So, the amount of current flowing through the electrical device is 6.3 watts divided by the voltage source in volts (Z).

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(a) To convert 105 Calories to joules, multiply by 4.184 J/cal.

(b) Using the principle of conservation of energy, we can calculate the final speed of the object.

(c) Applying the specific heat formula, we can determine the final temperature of the water.

To convert Calories to joules, we can use the conversion factor of 4.184 J/cal. Multiplying 105 Calories by 4.184 J/cal gives us the energy in joules.

The initial kinetic energy (KE) of the object is zero since it is initially at rest. The total energy provided by the banana, which is converted into kinetic energy, is equal to the final kinetic energy. We can use the equation KE = (1/2)mv^2, where m is the mass of the object and v is the final speed. Plugging in the known values, we can solve for v.

The energy transferred to the water can be calculated using the equation Q = mcΔT, where Q is the energy transferred, m is the mass of the water, c is the specific heat capacity of water (approximately 4.184 J/g°C), and ΔT is the change in temperature. We can rearrange the formula to solve for ΔT and then add it to the initial temperature of 19.7°C to find the final temperature.

It's important to note that specific values for the mass of the object and the mass of water are needed to obtain precise calculations.

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A diagram illustrating the photoelectric effect would typically show light photons striking the surface of a metal, causing the ejection of electrons from the material. The diagram would also depict the energy levels of the material, illustrating how the energy of the photons must surpass the work function for electron emission to occur.

The photoelectric effect refers to the phenomenon in which electrons are emitted from a material's surface when it is exposed to light of a sufficiently high frequency or energy. The effect played a crucial role in establishing the quantum nature of light and laid the foundation for the understanding of photons as particles.

Here's a simplified explanation of the photoelectric effect:

1. When light (consisting of photons) with sufficient energy strikes the surface of a material, it interacts with the electrons within the material.

2. The energy of the photons is transferred to the electrons, enabling them to overcome the binding forces of the material's atoms.

3. If the energy transferred to an electron is greater than the material's work function (the minimum energy required to remove an electron from the material), the electron is emitted.

4. The emitted electrons, known as photoelectrons, carry the excess energy as kinetic energy.

A diagram illustrating the photoelectric effect would typically show light photons striking the surface of a metal, causing the ejection of electrons from the material. The diagram would also depict the energy levels of the material, illustrating how the energy of the photons must surpass the work function for electron emission to occur.

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Answer:

True

Explanation:

If the electric potential is lower at P2 than at P1, then the work done by the electric force is positive.

Answer:

The answer to this I would say is True.

Explanation:

The work done by the electric force on a charge is given by the equation:

W = q(V2 - V1)

Where:

According to the question, V2 (the potential at P2) is lower than V1 (the potential at P1). Since the charge (q) is negative, this means that (V2 - V1) will be a positive number.

Plugging this into the work equation, we get:

W = -1 (V2 - V1)

Since (V2 - V1) is positive, this makes W positive as well.

Therefore, the statement is true - when the potential is lower at P2 than P1, and the charge is negative, the work done by the electric force will be positive. This is because the potential difference term (V2 - V1) in the work equation is positive, and the negative charge just makes the entire expression positive.

So in summary, when we use the actual work equation for electric force, W = q(V2 - V1), we can see that the statement in the question is true.