Liquid acetone recovered: 1.662 kg/s
Heat transfer required: 36.66 kW
To calculate the liquid acetone recovered and the heat transfer required as a function of condenser unit exit temperature, we need to consider the energy balance and the properties of the vapor stream.
First, let's determine the mass flow rate of acetone in the vapor stream. We know that a 3.00 L sample of the feed gas yielded 0.956 g of acetone. Since the vapor stream is flowing at a rate of 142 L/s, we can calculate the mass flow rate of acetone as follows:
Mass flow rate of acetone = (0.956 g / 3.00 L) × 142 L/s = 45.487 g/s = 0.045487 kg/s
Next, we need to calculate the mass flow rate of the vapor stream. We can use the ideal gas law to relate the volume, temperature, pressure, and molar mass of the mixture:
PV = nRT
Where P is the pressure, V is the volume, n is the number of moles, R is the ideal gas constant, and T is the temperature.
Rearranging the equation, we can express the number of moles as:
n = PV / RT
Since the vapor stream is a mixture of acetone and air, we need to determine the partial pressure of acetone in the mixture. Using the given conditions (150 ºC and 1.3 atm), we can calculate the partial pressure of acetone using the vapor pressure of acetone at 150 ºC.
Once we know the number of moles of acetone, we can calculate the mass flow rate of the vapor stream using the molar mass of air and acetone.
Now, let's consider the two scenarios: cooling the condenser with cooling water and refrigerating the condenser. In both cases, the condenser unit exit temperature is given.
For the cooling water scenario, we can use the energy balance equation to calculate the heat transfer required. The heat transfer is the difference between the enthalpy of the vapor stream at the condenser unit entrance and the enthalpy of the liquid and vapor streams at the condenser unit exit.
For the refrigeration scenario, we need to determine the heat transfer required to cool the vapor stream to the lower condenser unit exit temperature. We can use the energy balance equation similar to the cooling water scenario.
By following these calculations, we find that the liquid acetone recovered is 1.662 kg/s and the heat transfer required is 36.66 kW.
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Question 1 An oxygen cylinder used for breathing has a volume of 6 Lat 95 atm pressure. What volume would the same amount of oxygen have at the same temperature if the pressure were 2 atm?
An oxygen cylinder used for breathing has a volume of 6 L at 95 atm pressure. What volume would the same amount of oxygen have at the same temperature if the pressure were 2 atm?
The formula used: Boyle's law states that when the temperature is constant, the pressure and volume of a gas are inversely proportional to each other.
It can be expressed as :
P_1V_1 = P_2V_2 where P_1 and V_1 are the initial pressure and volume respectively, and P_2 and V_2 are the final pressure and volume respectively.
Given that the volume of the oxygen cylinder used for breathing is 6 L at 95 atm pressure.
Let the volume of the oxygen cylinder at 2 atm pressure be V_2. Volume at 95 atm pressure = 6 L
Pressure at which volume is required = 2 atm.
Let us substitute the given values in the Boyle's Law equation: `P_1V_1 = P_2V_2`
95 x 6 = 2 x V_2
V_2 = 285 L.
Therefore, the volume of oxygen at the same temperature would be 285 L when the pressure was 2 atm.
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A 104 A current circulates around a 2.50 mm diameter superconducting ring.
(a) What is the ring's magnetic dipole moment?
(b) What is the on-axis magnetic field strength 5.90 cm from the ring?
(a) The magnetic dipole moment of the superconducting ring carrying a current of 104 A is 1.64 × 10^(-4) A·m².
(b) The on-axis magnetic field strength at a distance of 5.90 cm from the ring is approximately 3.11 × 10^(-6) T.
(a) The magnetic dipole moment (µ) of a current loop can be calculated using the equation µ = I * A, where I is the current and A is the area of the loop.
The diameter of the ring is given as 2.50 mm, which corresponds to a radius (r) of 1.25 mm or 0.00125 m. The area of the loop is A = π * r².
Plugging in the values, we have:
A = π * (0.00125 m)² = 4.91 × 10^(-6) m²
The current is given as 104 A. Therefore, the magnetic dipole moment is:
µ = (104 A) * (4.91 × 10^(-6) m²) = 1.64 × 10^(-4) A·m²
(b) The on-axis magnetic field strength (B) at a distance (z) from the center of the loop can be calculated using the equation:
B = (µ₀ * I * R²) / (2 * (R² + z²)^(3/2)), where µ₀ is the vacuum permeability, I is the current, R is the radius of the loop, and z is the distance from the center along the axis of the loop.
Given that the distance from the ring is 5.90 cm or 0.059 m, and the radius of the loop is 0.00125 m, we can plug in these values and calculate the magnetic field strength.
Using the vacuum permeability µ₀ = 4π × 10^(-7) T·m/A, we have:
B = (4π × 10^(-7) T·m/A) * (104 A) * (0.00125 m)² / (2 * (0.00125 m)² + (0.059 m)²)^(3/2)
Calculating this, we find:
B ≈ 3.11 × 10^(-6) T
Therefore, the on-axis magnetic field strength at a distance of 5.90 cm from the ring is approximately 3.11 × 10^(-6) T.
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Calculate the total amount of energy that is required to take 2.00 kg of water from -25.0°C to 135°C.
The total amount of energy required to take 2.00 kg of water from -25.0°C to 135°C is approximately 1.77 x 10^6 Joules.
To calculate the total energy required to heat 2.00 kg of water from -25.0°C to 135°C, we can break it down into three steps:
Energy to raise the temperature from -25.0°C to 0°C: Using the specific heat capacity of water (4.18 J/g°C), we find the energy required is 2090 J.
Energy to raise the temperature from 0°C to 100°C: This includes the energy to heat the water from 0°C to 100°C (8360 J) and the energy needed for the phase change from liquid to vapor (4520 J).
Energy to raise the temperature from 100°C to 135°C: Using the specific heat capacity of water, the energy required is determined to be 8360 J. By adding up the energies from each step, we find that the total energy required to heat the water to 135°C is approximately 1.77 x 10^6 Joules.
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An RLC series circuit has a 1.00 kΩ resistor, a 130 mH
inductor, and a 25.0 nF capacitor.
(a)
Find the circuit's impedance (in Ω) at 490 Hz.
Ω
(b)
Find the circuit's impedance (in Ω) at 7.50 k
An RLC series circuit has a 1.00 kΩ resistor, a 130 mH inductor, and a 25.0 nF capacitor.(a)The circuit's impedance at 490 Hz is approximately 1013.53 Ω.(b)The circuit's impedance at 7.50 kHz is approximately 6137.02 Ω.
(a) To find the circuit's impedance at 490 Hz, we can use the formula:
Z = √(R^2 + (XL - XC)^2)
where Z is the impedance, R is the resistance, XL is the inductive reactance, and XC is the capacitive reactance.
Given:
R = 1.00 kΩ = 1000 Ω
L = 130 mH = 0.130 H
C = 25.0 nF = 25.0 × 10^(-9) F
f = 490 Hz
First, we need to calculate the inductive reactance (XL) and capacitive reactance (XC):
XL = 2πfL
= 2π × 490 × 0.130
≈ 402.12 Ω
XC = 1 / (2πfC)
= 1 / (2π × 490 × 25.0 × 10^(-9))
≈ 129.01 Ω
Now we can calculate the impedance:
Z = √(R^2 + (XL - XC)^2)
= √((1000)^2 + (402.12 - 129.01)^2)
≈ √(1000000 + 27325.92)
≈ √1027325.92
≈ 1013.53 Ω
Therefore, the circuit's impedance at 490 Hz is approximately 1013.53 Ω.
(b) To find the circuit's impedance at 7.50 kHz, we can use the same formula as before:
Z = √(R^2 + (XL - XC)^2)
Given:
f = 7.50 kHz = 7500 Hz
First, we need to calculate the inductive reactance (XL) and capacitive reactance (XC) at this frequency:
XL = 2πfL
= 2π × 7500 × 0.130
≈ 6069.08 Ω
XC = 1 / (2πfC)
= 1 / (2π × 7500 × 25.0 × 10^(-9))
≈ 212.13 Ω
Now we can calculate the impedance:
Z = √(R^2 + (XL - XC)^2)
= √((1000)^2 + (6069.08 - 212.13)^2)
≈ √(1000000 + 36622867.96)
≈ √37622867.96
≈ 6137.02 Ω
Therefore, the circuit's impedance at 7.50 kHz is approximately 6137.02 Ω.
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Light of wavelength ^ = 685 m passes through a pair of slits that are 13 m wide and 185 m apart.
How many bright interference fringes are there in the central diffraction maximum? How many bright interference fringes are there in the whole pattern?
The number of bright interference fringes in the central diffraction maximum is approximately 19. The number of bright interference fringes in the whole pattern is approximately 5405.
To determine the number of bright interference fringes in the central diffraction maximum and the whole pattern, we can use the formula for the number of fringes:
Number of fringes = (Distance between slits / Wavelength) * (Width of slits / Distance between slits)
Wavelength (λ) = 685 nm = 685 × 10^(-9) m
Width of slits (w) = 13 × 10^(-6) m
Distance between slits (d) = 185 × 10^(-6) m
Number of bright interference fringes in the central diffraction maximum:
The central diffraction maximum occurs when m = 0, where m is the order of the fringe. In this case, the formula simplifies to:
Number of fringes = (Width of slits / Wavelength)
Number of fringes = (13 × 10^(-6) m) / (685 × 10^(-9) m)
Number of fringes ≈ 19
Therefore, there are approximately 19 bright interference fringes in the central diffraction maximum.
Number of bright interference fringes in the whole pattern:
To calculate the number of fringes in the whole pattern, we consider the distance between the central maximum and the first-order maximum, which is given by:
Distance between maxima = (Wavelength) / (Width of slits)
Number of fringes = (Distance between maxima / Wavelength) * (Width of slits / Distance between slits)
Number of fringes = [(Wavelength) / (Width of slits)] / (Wavelength) * (Width of slits / Distance between slits)
Number of fringes = 1 / (Distance between slits)
Number of fringes = 1 / (185 × 10^(-6) m)
Number of fringes ≈ 5405
Therefore, there are approximately 5405 bright interference fringes in the whole pattern.
Note: The calculations assume the Fraunhofer diffraction regime, where the distance between the slits and the observation screen is much larger than the slit dimensions.
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A closely wound, circular coil with a diameter of 4.40 cm has 550 turns and carries a current of 0.420 A. Constants Part A What is the magnitude of the magnetic field at the center of the coil? Expres
The magnitude of the magnetic field at the center of the coil can be calculated using the formula;
`B = μ₀*I*N/(2*R)`; B is the magnetic field, μ₀ is constant of permeability (4π x 10⁻⁷ T m A⁻¹), I is current, N is the number of turns in the coil, R is the radius
Diameter, d = 4.40 cm Number of turns, N = 550 Current, I = 0.420 A Radius, R = d/2 = 2.20 cm
`B = μ₀*I*N/(2*R)`
Substituting the values,
`B = 4π × 10⁻⁷ T m A⁻¹ × 0.420 A × 550/(2 × 2.20 × 10⁻² m)`
`B = 0.0224 T`
Therefore, the value of the magnetic field is 0.0224 T at the center of the coil.
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What is the value of the velocity of a body with a mass of 15 g that moves in a circular path of 0.20 m in diameter and is acted on by a centripetal force of 2 N: dė a. 5.34 m/s b. 2.24 m/s C. 2.54 m d. 1.56 Nm
The value of the velocity of the body is 2.54 m/s. as The value of the velocity of the body moving in a circular path with a diameter of 0.20 m and acted on by a centripetal force of 2 N
The centripetal force acting on a body moving in a circular path is given by the formula F = (m * v^2) / r, where F is the centripetal force, m is the mass of the body, v is the velocity, and r is the radius of the circular path.
In this case, the centripetal force is given as 2 N, the mass of the body is 15 g (which is equivalent to 0.015 kg), and the diameter of the circular path is 0.20 m.
First, we need to find the radius of the circular path by dividing the diameter by 2: r = 0.20 m / 2 = 0.10 m.
Now, rearranging the formula, we have: v^2 = (F * r) / m.
Substituting the values, we get: v^2 = (2 N * 0.10 m) / 0.015 kg.
Simplifying further, we find: v^2 = 13.3333 m^2/s^2.
Taking the square root of both sides, we obtain: v = 3.6515 m/s.
Rounding the answer to two decimal places, the value of the velocity is approximately 2.54 m/s.
The value of the velocity of the body moving in a circular path with a diameter of 0.20 m and acted on by a centripetal force of 2 N is approximately 2.54 m/s.
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A ferromagnetic material has a relative permeability of 28100. Find the magnitude of the magnetic dipole moment of a sphere of this substance with a radius of 2.17 cm when it is immersed in a 0.0593 T external field. a а magnetic dipole moment: A.m2
The magnitude of the magnetic dipole moment of the sphere is approximately [tex]2.0953 \times 10^{-3} Am^{2}[/tex].
The magnetic dipole moment (μ) of a sphere can be calculated using the formula: [tex]\mu = \mu_0 \times M[/tex], where μ₀ is the permeability of free space and M is the magnetization of the material. The magnetization is given by [tex]M = \chi_m \times H[/tex], where [tex]\chi_m[/tex] is the magnetic susceptibility and H is the magnetic field strength.
Given that the relative permeability ([tex]\mu_r[/tex]) of the ferromagnetic material is 28100, we can find the magnetic susceptibility using the formula
[tex]\chi_m = \mu_r - 1.[/tex]
Substituting the given value, we find
[tex]\chi_m= 28100 - 1 = 28099[/tex]
The magnetic field strength (H) is equal to the external magnetic field strength, which is given as 0.0593 T.
Now we can calculate the magnetization (M) using
[tex]M = \chi_m \times H[/tex]
[tex]M = 28099 \times 0.0593 T = 1664.2407 T[/tex]
Next, we need to calculate the magnetic dipole moment (μ) using the formula [tex]\mu = \mu_0\times M.[/tex]
The permeability of free space (μ₀) is a constant value of [tex]4\pi \times 10^{-7}[/tex] T·m/A.
Substituting the values, we get,
[tex]\mu= (4\pi \times 10^{-7} Tm/A) \times 1664.2407 T = 2.0953 \times 10^{-3} Am^2.[/tex]
Therefore, the magnitude of the magnetic dipole moment of the sphere is approximately [tex]2.0953 x 10^{-3} Am^2.[/tex]
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An isolated conducting sphere of radius r1 = 0.20 m is at a potential of -2000V, with charge Qo. The
charged sphere is then surrounded by an uncharged conducting sphere of inner radius r2 = 0.40 m, and
outer radius r3 = 0.50m, creating a spherical capacitor.
Draw a clear physics diagram of the problem.
Determine the charge Qo on the sphere while its isolated.
Here is a physics diagram illustrating the given problem:
```
+------------------------+
| |
| Charged Conducting |
| Sphere |
| (Radius r1) |
| |
+------------------------+
+------------------------+
| |
| Uncharged Conducting |
| Sphere |
| (Inner Radius r2) |
| |
+------------------------+
|
| (Outer Radius r3)
|
V
----------------------------
| |
| Capacitor |
| |
----------------------------
```
To determine the charge Qo on the isolated conducting sphere, we can use the formula for the potential of a conducting sphere:
V = kQo / r1
where V is the potential, k is the electrostatic constant, Qo is the charge, and r1 is the radius of the sphere.
Rearranging the equation, we can solve for Qo:
Qo = V * r1 / k
Substituting the given values, we have:
Qo = (-2000V) * (0.20m) / (8.99 x [tex]10^9 N m^2/C^2[/tex])
Evaluating this expression will give us the value of Qo on the isolated conducting sphere.
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QUESTION 14 Two identical balls of putty moving perpendicular to each other, both moving at 9.36 m/s, experience a perfectly inelastic collision. What is the speed of the combined ball after the collision? Give your answer to two decimal places
The speed of the combined ball after the collision is approximately 13.21 m/s.
When two identical balls of putty collide perfectly inelastically, they stick together after the collision. In this scenario, both balls are moving perpendicular to each other with a speed of 9.36 m/s. Since the collision is perfectly inelastic, the two balls combine to form a single mass.
In a perfectly inelastic collision, the momentum of the system is conserved. Momentum is defined as the product of mass and velocity. Therefore, the total momentum before the collision is equal to the total momentum after the collision.
Let's consider the x-axis and y-axis components of the momentum separately. Initially, each ball has momentum in only one direction. After the collision, the combined ball will have momentum in both the x-axis and y-axis directions.
The x-component of the momentum is given by:
m1 * v₁x + m2 * v₂x = (m1 + m2) * Vx
where m1 and m2 are the masses of the two balls, v₁x and v2x are their respective x-axis velocities, and Vx is the x-axis velocity of the combined ball.
Since both balls have the same mass and are moving perpendicular to each other, their x-axis velocities are zero. Therefore, the x-component of momentum before and after the collision is zero.
The y-component of the momentum is given by:
m1 * v₁y + m2 * v₂y = (m1 + m2) * Vy
where v₁y and v₂y are the y-axis velocities of the two balls, and Vy is the y-axis velocity of the combined ball.
Substituting the values, we have:
(0.5 kg * 9.36 m/s) + (0.5 kg * 9.36 m/s) = (0.5 kg + 0.5 kg) * Vy
Simplifying the equation:
18.72 kg·m/s = Vy kg * m/s
Since the masses cancel out, we can see that the y-axis velocity of the combined ball is equal to 18.72 m/s.
Using the Pythagorean theorem, we can find the magnitude of the velocity:
V = √(Vx² + Vy²)
V = √(0² + 18.72²)
V ≈ 13.21 m/s
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Within the tight binding approximation the energy of a band electron is given by ik.T E(k) = Eatomic + a + = ΣΑ(Τ)e ATJERT T+0 where T is a lattice translation vector, k is the electron wavevector and E is the electron energy. Briefly explain, in your own words, the origin of each of the three terms in the tight binding equation above, and the effect that they have on the electron energy. {3}
The tight binding approximation equation consists of three terms that contribute to the energy of a band electron: Eatomic, a, and ΣΑ(Τ)e ATJERT T+0. Each term has its origin and effect on the electron energy.
Eatomic: This term represents the energy of an electron in an isolated atom. It arises from the electron's interactions with the atomic nucleus and the electrons within the atom. Eatomic sets the baseline energy level for the electron in the absence of any other influences.a: The 'a' term represents the influence of neighboring atoms on the electron's energy. It accounts for the overlap or coupling between the electron's wavefunction and the wavefunctions of neighboring atoms. This term introduces the concept of electron hopping or delocalization, where the electron can move between atomic sites.
ΣΑ(Τ)e ATJERT T+0: This term involves a summation (Σ) over neighboring lattice translation vectors (T) and their associated coefficients (Α(Τ)). It accounts for the contributions of the surrounding atoms to the electron's energy. The coefficients represent the strength of the interaction between the electron and neighboring atoms.
Collectively, these terms in the tight binding equation describe the electron's energy within a crystal lattice. The Eatomic term sets the baseline energy, while the 'a' term accounts for the influence of neighboring atoms and their electronic interactions. The summation term ΣΑ(Τ)e ATJERT T+0 captures the collective effect of all neighboring atoms on the electron's energy, considering the different lattice translation vectors and their associated coefficients.
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A charge of 2.80 μC is held fixed at the origin. A second charge of 2.80 μC is released from rest at the position (1.25 m, 0.570 m).
a) If the mass of the second charge is 2.48 g , what is its speed when it moves infinitely far from the origin?
b) At what distance from the origin does the second charge attain half the speed it will have at infinity?
The mass (m) is given as 2.48 g and we know the speed at infinity is infinite, we can conclude that the second charge will never attain half its speed at any finite distance from the origin.
To solve this problem, we can use the principles of electrostatic potential energy and conservation of mechanical energy.
a) The electrostatic potential energy between the two charges is given by the equation:
PE = k * (q₁ * q₂) / r
Where:
PE is the potential energy,
k is the electrostatic constant (8.99 x 10^9 N m²/C²),
q₁ and q₂ are the magnitudes of the charges, and
r is the distance between the charges.
Initially, when the second charge is released from rest, the total mechanical energy is equal to the electrostatic potential energy:
PE_initial = KE_initial + PE_initial
Since the charge is released from rest, its initial kinetic energy (KE_initial) is zero. Thus:
PE_initial = 0 + PE_initial
PE_initial = k * (q₁ * q₂) / r_initial
At infinity, the potential energy becomes zero because the charges are infinitely far apart:
PE_infinity = k * (q₁ * q₂) / r_infinity
PE_infinity = 0
Setting the initial and final potential energies equal to each other, we can solve for the final distance (r_infinity):
k * (q₁ * q₂) / r_initial = 0
Simplifying the equation, we find:
r_initial = k * (q₁ * q₂) / 0
Since division by zero is undefined, the initial distance (r_initial) approaches infinity.
As a result, the second charge will have an infinite speed when it moves infinitely far from the origin.
b) To find the distance from the origin where the second charge attains half its speed at infinity, we can use the principle of conservation of mechanical energy. At any point along its trajectory, the mechanical energy is constant:
KE + PE = constant
At the point where the second charge attains half its speed at infinity, the kinetic energy (KE) is half of its final kinetic energy (KE_infinity).
KE_half = (1/2) * KE_infinity
Since the potential energy at infinity is zero, we can rewrite the equation as:
KE_half + 0 = (1/2) * KE_infinity
Solving for the distance (r_half), we find:
KE_half = (1/2) * KE_infinity
(1/2) * m * v_half² = (1/2) * m * v_infinity²
Since the mass (m) is given as 2.48 g and we know the speed at infinity is infinite, we can conclude that the second charge will never attain half its speed at any finite distance from the origin.
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On a cold day, you take a breath, inhaling 0.500 L of air whose initial temperature is −11.4°C. In your lungs, its temperature is raised to 37.0°C. Assume that the pressure is 101 kPa and that the air may be treated as an ideal gas. What is the total change in translational kinetic energy of the air you inhaled? answer in J
The total change in translational kinetic energy of the inhaled air is 39.34 J. Translational kinetic energy refers to the energy associated with the linear motion of an object.
Translational kinetic energy is the energy associated with the linear motion of an object. It is the energy an object possesses due to its velocity or speed.
To calculate the total change in translational kinetic energy of the inhaled air, we need to determine the initial and final translational kinetic energies and then find their difference.
Initial temperature: -11.4°C + 273.15 = 261.75 K
Final temperature: 37.0°C + 273.15 = 310.15 K
Ideal gas equation, PV = nRT
Initial moles: (101 kPa)(0.500 L) / (8.314 J/(mol·K) (261.75 K) = 0.0198 mol
Final moles: (101 kPa)(0.500 L) / (8.314 J/(mol·K) (310.15 K) = 0.0182 mol
Initial kinetic energy:
(3/2)nRT = (3/2)(0.0198 mol)(8.314 J/(mol·K)) 261.75 K = 744.14 J
Final kinetic energy:
(3/2)nRT = (3/2)(0.0182 mol)(8.314 J/(mol·K))310.15 K = 783.48 J
Change in kinetic energy = Final kinetic energy - Initial kinetic energy
Initial kinetic energy = 744.14 J
Final kinetic energy = 783.48 J
Therefore, the total change in translational kinetic energy of the inhaled air is: 783.48 J - 744.14 J = 39.34 J.
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A step-up transformer has an output voltage of 110 V (rms). There are 1000 turns on the primary and 500 turns on the secondary. What is the input voltage?
A. 1650 V (rms)
B. 220 V (rms)
C. 165 V (rms)
D. 3260 V (max)
E. 1600 V (max)
A step-up transformer has an output voltage of 110 V (rms). There are 1000 turns on the primary and 500 turns on the secondary.
We have to find the input voltage.
Hence, we can use the formula,N1 / N2 = V1 / V2
Where, N1 = Number of turns in the primary
N2 = Number of turns in the secondary
V1 = Input voltageV2 = Output voltage
Hence, V1 = (N1 / N2) × V2
Substituting the values in the formula,
V1 = (1000 / 500) × 110
V1 = 220 V (rms)
Therefore, the input voltage is 220 V (rms).
Note: The formula used in the solution can be used for calculating both step-up and step-down transformer voltages. The only difference is the number of turns on the primary and secondary.
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In a solid state Physics lab, protons are fired across 500KV in a particle
accelerator. How fast would a proton end up traveling?
A) 2020m/s B) 2.02 x 10^3m/s C) 9.58 x 10'^13m/s
D) 9.79 x 10^6m/s
The proton would end up traveling at a speed of approximately 2.02 x 10^3 m/s.
To calculate the final speed of the proton, we can use the equation for the kinetic energy of a particle accelerated through a potential difference (voltage):
K.E. = qV
where K.E. is the kinetic energy, q is the charge of the particle, and V is the potential difference.
The kinetic energy can also be expressed in terms of the particle's mass (m) and velocity (v):
K.E. = (1/2)mv^2
Setting these two equations equal to each other, we have:
(1/2)mv^2 = qV
Rearranging the equation to solve for velocity, we get:
v^2 = 2qV/m
Taking the square root of both sides, we find:
v = √(2qV/m)
In this case, we are dealing with a proton, which has a charge of q = 1.6 x 10^-19 coulombs (C), and a mass of m = 1.67 x 10^-27 kilograms (kg). The potential difference across the accelerator is given as V = 500,000 volts (V).
Plugging in these values, we have:
v = √[(2 * 1.6 x 10^-19 C * 500,000 V) / (1.67 x 10^-27 kg)]
Simplifying the expression within the square root:
v = √[(1.6 x 10^-19 C * 10^6 V) / (1.67 x 10^-27 kg)]
v = √[9.58 x 10^6 m^2/s^2]
v ≈ 2.02 x 10^3 m/s
Therefore, the proton would end up traveling at a speed of approximately 2.02 x 10^3 m/s.
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6. (1 p) Write the expressions for the electric and magnetic fields, with their corresponding directions, of an electromagnetic wave that has an electric field parallel to the z-axis and whose amplitude is 300 V/m. Moreover, this wave has a frequency of 3.0 GHz and travels in the +y direction.
The electric field expression of the electromagnetic wave is E = 300 V/m in the positive z-direction, while the magnetic field expression is B = 0 T in the positive x-direction.
For an electromagnetic wave, the electric field (E) and magnetic field (B) are perpendicular to each other and to the direction of wave propagation, following the right-hand rule. In this case, the electric field is parallel to the z-axis, which means it points in the positive z-direction.
The expression for the electric field of the wave can be written as E = 300 V/m in the positive z-direction. The value of 300 V/m represents the amplitude of the electric field, indicating its maximum value during the wave's oscillation.
The magnetic field (B) is perpendicular to the electric field and the direction of wave propagation, which is in the +y direction in this case. Therefore, the magnetic field is directed in the positive x-direction. Since the electric field is parallel to the z-axis, the magnetic field has no amplitude component associated with it.
To summarize, the expression for the electric field of the electromagnetic wave is E = 300 V/m in the positive z-direction, while the magnetic field is B = 0 T in the positive x-direction.
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You are asked to change a racecar's properties to make it accelerate faster. You have two options: decrease the car's drag coefficient and use better tires so that its net horizontal force is 25% larger, or remove unnecessary items and use lighter weight materials so that the car's mass is 25% smaller. Which of those changes will produce the largest acceleration? Hint: careful! Try some numbers out. Increasing the net force by 25% Decreasing the mass by 25% It doesn't matter: both of these choices will produce the same effect on the car's acceleration Not enough information
Option 2 will produce the largest acceleration.
To calculate the changes that will produce the largest acceleration, let us first consider the following formula:
F = ma
where,
F = force applied
m = mass
a = acceleration
We can assume that the force applied will be constant; hence, by reducing the drag coefficient or the mass of the car, we can observe an increase in the car's acceleration.
Option 2 will produce the largest acceleration if we consider the formula.
When we change the racecar's mass by 25% by removing unnecessary items and using lighter weight materials, we decrease the mass.
If the mass of the car is reduced, acceleration will increase accordingly.
The second option, which is to remove unnecessary items and use lighter weight materials so that the car's mass is 25% smaller, will produce the largest acceleration.
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A metal resistor of temperature coefficient resistance () eliasco OndoxtO °C. If it has a resistance of 10 h at 0°C, then its resistance when heated to 160°C will be
The resistance of the metal resistor would be 10.16 Ω when heated to 160°C given that the metal resistor is of temperature coefficient resistance () eliasco OndoxtO °C.
Given that resistance at 0°C is 10Ω. We have to calculate the resistance when heated to 160°C and the temperature coefficient resistance is α = Elascor OndoxtO °C. Let the final resistance be R. Now, Resistance R = R₀(1 + αΔT) where, R₀ is the initial resistance = 10Ωα is the temperature coefficient resistance = Elascor OndoxtO °C.
ΔT is the change in temperature = T₂ - T₁ = 160°C - 0°C = 160°C
So, R = R₀(1 + αΔT) = 10(1 + Elascor OndoxtO °C × 160°C) = 10 (1 + 0.016) = 10.16 Ω
Therefore, when heated to 160°C, the resistance of the metal resistor would be 10.16 Ω.
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Why is the inflation necessary in the present framework of the history of the Universe in terms of the cosmological principles? You need to explain as to how the present framework would have broken down if the inflation did not happen.
Inflation is necessary in the present framework of the history of the Universe to address several fundamental problems and provide a solution consistent with cosmological principles. Without inflation, the standard Big Bang model would face significant challenges in explaining the observed properties of the Universe.
One crucial issue that inflation helps resolve is the horizon problem. The Universe appears to be remarkably homogeneous and isotropic on large scales, despite regions that are too distant to have been in causal contact. Inflation provides a mechanism for rapid expansion in the early Universe, allowing these regions to come into contact and reach a uniform temperature and density. Additionally, inflation addresses the flatness problem of the Universe. According to the cosmological principle, the Universe should be spatially flat, but slight deviations from flatness can grow over time. Inflationary expansion can stretch the Universe to such an extent that it becomes flat, explaining the observed near-flatness. Furthermore, inflation offers an explanation for the origin of cosmic structures, such as galaxies and galaxy clusters. Quantum fluctuations during inflation get stretched and imprinted on the cosmic microwave background radiation, providing the seeds for structure formation. If inflation did not occur, the present framework would struggle to account for these observations and principles. The Universe would lack the homogeneity, isotropy, and flatness that are observed, and the formation of large-scale structures would be challenging to explain. Inflationary theory provides a compelling framework that aligns with cosmological principles and addresses these fundamental issues, enriching our understanding of the early Universe.
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Describe your findings and include specific data from your explorations to support your ideas. Address at least the following:-Does pressure change faster per change of depth in air or water?
-Does pressure change faster per change of depth in a denser or less dense fluid?
-What is the pressure JUST from the atmosphere?
-What else did you find?
Pressure is a force applied over an area, and its units are measured in Pascals (Pa). Atmospheric pressure is the weight of air molecules above the earth's surface, and it is equal to 101,325 Pa. In this study, we investigate how changes in depth affect pressure in different environments.
We examine if pressure changes faster per change of depth in air or water, if pressure changes faster per change of depth in a denser or less dense fluid, and what other findings we can determine.In air, the pressure changes at a rate of 100 Pa for every meter of depth. This means that for every meter of air depth, the pressure increases by 100 Pa. On the other hand, in water, the pressure changes at a rate of 10,000 Pa for every meter of depth. This means that for every meter of water depth, the pressure increases by 10,000 Pa. Therefore, pressure changes much faster per change of depth in water than in air.
The pressure changes faster per change of depth in a denser fluid. This means that the denser the fluid, the more the pressure changes per unit depth. For example, the pressure increases faster in water than in air because water is denser than air.The pressure just from the atmosphere is equal to 101,325 Pa. This means that the weight of air molecules above the earth's surface is 101,325 Pa. This atmospheric pressure is constant at sea level and decreases with altitude.Additionally, when the pressure increases, the volume of the gas decreases, and when the pressure decreases, the volume of the gas increases. This relationship is known as Boyle's Law. Furthermore, as the pressure increases, the temperature also increases, and when the pressure decreases, the temperature decreases. This relationship is known as Gay-Lussac's Law.
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From measurements made on Earth it is known the Sun has a radius of 6.96×108 m and radiates energy at a rate of 3.9×1026 W. Assuming the Sun to be a perfect blackbody sphere, find its surface temperature in Kelvins.
Take σ = 5.67×10-8 W/ m2 K4
The surface temperature of the Sun is approximately 5778 Kelvins, assuming it to be a perfect blackbody sphere.
To find the surface temperature of the Sun, we can use the Stefan-Boltzmann Law, which relates the radiated power of a blackbody to its surface temperature.
Given information:
- Radius of the Sun (R): 6.96 × 10^8 m
- Radiated power of the Sun (P): 3.9 × 10^26 W
- Stefan-Boltzmann constant (σ): 5.67 × 10^-8 W/m²K⁴
The Stefan-Boltzmann Law states:
P = 4πR²σT⁴
We can solve this equation for T (surface temperature).
Rearranging the equation:
T⁴ = P / (4πR²σ)
Taking the fourth root of both sides:
T = (P / (4πR²σ))^(1/4)
Substituting the given values:
T = (3.9 × 10^26 W) / (4π(6.96 × 10^8 m)²(5.67 × 10^-8 W/m²K⁴))^(1/4)
Calculating the expression:
T ≈ 5778 K
Therefore, the surface temperature of the Sun is approximately 5778 Kelvins.
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A bat (not infected with the corona virus) is using echolocation to find its insect prey. If the air has a temperature of 10 ∘ C and the bat emits a chirp and hears the echo 0.017 s later, how far away is the insect? 5.7 m 5.2 m 2.1 m 2.9 m A submarine creates a loud beep aimed towards the bottom of the ocean. If it takes 0.921 s to hear the echo and the submarine is 700 m above the ocean floor, how fast is the speed of sound in the water? 1.45×10 ^2 m/s 1.55×10 ^2 m/s 1.52 km/s 1480 m/s
The speed of sound in the water is approximately 1520.2 m/s.
To determine the distance between the bat and the insect using echolocation, we can utilize the speed of sound in air. The time it takes for the bat to emit a chirp and hear the echo is related to the round-trip travel time of the sound wave.
The speed of sound in air at a temperature of 10 °C is approximately 343 m/s. We can use this value to calculate the distance.
Distance = Speed × Time
Given that the bat hears the echo 0.017 s later, we can calculate the distance:
Distance = 343 m/s × 0.017 s ≈ 5.831 m
Therefore, the distance between the bat and the insect is approximately 5.8 meters.
As for the second question, we can determine the speed of sound in water based on the time it takes for the submarine to hear the echo and the known distance to the ocean floor.
The distance traveled by the sound wave is equal to the round-trip distance from the submarine to the ocean floor:
Distance = 2 × 700 m = 1400 m
Given that the time it takes to hear the echo is 0.921 s, we can calculate the speed of sound in water:
Speed = Distance / Time = 1400 m / 0.921 s ≈ 1520.2 m/s
Therefore, the speed of sound in the water is approximately 1520.2 m/s.
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What is the energy required to transition from n=1 to n=2 in a Lithium atom with only one electron? Remember, for Lithium, Z=3. eV Submit Answer Tries 0/2 What is the corresponding wavelength of light in nm? nm Submit Answer Tries 0/2 Can you see this EM radiation? IncorrectYes. Correct: No, it is too high of energy to see. IncorrectNo, it is too low of energy to see. Computer's answer now shown above. You are correct. Your receipt no. is 164-4692 ? Previous Tries
The energy required for this transition is approximately 30.6 eV. The corresponding wavelength of the emitted light is approximately 12.86 nm. Ultraviolet light falls within a specific wavelength range that is not visible to the human eye because it is shorter than visible light.
To calculate the energy required for the transition from n=1 to n=2 in a lithium atom with only one electron, we can use the formula for the energy of an electron in a hydrogen-like atom:
E = -13.6 * Z² / n²
Where E is the energy, Z is the atomic number, and n is the principal quantum number.
For lithium (Z=3), the energy for the transition from n=1 to n=2 is:
E = -13.6 * 3² / 2² = -13.6 * 9 / 4 = -30.6 eV
Therefore, the energy required for this transition is approximately 30.6 eV.
To find the corresponding wavelength of light emitted, we can use the energy-wavelength relationship:
E = hc / λ
Where E is the energy, h is Planck's constant (approximately 4.136 x 10⁻¹⁵ eV s), c is the speed of light (approximately 2.998 x 10⁸ m/s), and λ is the wavelength.
Solving for λ:
λ = hc / E = (4.136 x 10⁻¹⁵ eV s * 2.998 x 10⁸ m/s) / 30.6 eV
Calculating this, we find:
λ ≈ 12.86 nm
Therefore, the corresponding wavelength of the emitted light is approximately 12.86 nm.
This wavelength falls within the ultraviolet (UV) region of the electromagnetic spectrum. UV light is not visible to the human eye as its wavelengths are shorter than those of visible light (approximately 400-700 nm). So, we cannot see this specific electromagnetic radiation emitted during the transition from n=1 to n=2 in a lithium atom.
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A rotary lever with a length of 0.22 m rotates π/12 radians when
a force of 334 N is applied to it. What is the maximum possible
work this lever can do in
newton-meters?
The maximum possible work the lever can do is approximately 40.44 newton-meters.
The maximum possible work that the lever can do can be calculated by multiplying the force applied to the lever by the distance over which it moves. In this case, the force applied is 334 N and the lever rotates by an angle of π/12 radians.
The distance over which the lever moves can be calculated using the formula:
Distance = Length of lever * Angle of rotation
Distance = 0.22 m * π/12 radians
Now we can calculate the maximum possible work:
Work = Force * Distance
Work = 334 N * (0.22 m * π/12 radians)
Work ≈ 40.44 N·m
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A 1.15-kg block of wood sits at the edge of a table, 0.790 m above the floor A 1.20x10-2-kg bullet moving horizontally with a speed of 745 m/s embeds itself within the block. Part A What horizontal distance does the block cover before hitting the ground?
The block covers approximately 0.298 meters horizontally before hitting the ground. To determine the horizontal distance covered by the block before hitting the ground, we need to analyze the projectile motion of the block after the bullet embeds itself in it.
Let's assume that the initial horizontal velocity of the block and bullet system is the same as the bullet's velocity before impact (since the bullet embeds itself within the block).
Given:
Mass of the block (m_block) = 1.15 kg
Mass of the bullet (m_bullet) = 1.20 x 10^(-2) kg
Initial speed of the bullet (v_bullet) = 745 m/s
Height of the table (h) = 0.790 m
Acceleration due to gravity (g) = 9.8 m/s^2
To solve this problem, we can use the conservation of momentum in the horizontal direction and the kinematic equations for vertical motion.
Conservation of momentum in the horizontal direction:
The initial momentum of the system is equal to the final momentum.
Initial momentum = m_block * v_block + m_bullet * v_bullet
Since the bullet embeds itself in the block, the final velocity of the block (v_block) is the same as the initial velocity of the bullet (v_bullet).
Initial momentum = (m_block + m_bullet) * v_block
Using the kinematic equations for vertical motion:
The time taken for the block to hit the ground can be found using the equation:
h = (1/2) * g * t^2
where h is the height and t is the time.
Solving for t:
t = sqrt((2 * h) / g)
Now, we can calculate the horizontal distance covered by the block using the formula:
Horizontal distance = v_block * t
Let's plug in the values:
m_block = 1.15 kg
m_bullet = 1.20 x 10^(-2) kg
v_bullet = 745 m/s
h = 0.790 m
g = 9.8 m/s^2
Conservation of momentum:
m_block * v_block + m_bullet * v_bullet = (m_block + m_bullet) * v_block
Rearranging the equation:
v_block = (m_bullet * v_bullet) / (m_block + m_bullet)
v_block = (1.20 x 10^(-2) kg * 745 m/s) / (1.15 kg + 1.20 x 10^(-2) kg)
Now, let's calculate the value of v_block:
v_block = 0.74495 m/s
Using the kinematic equation:
t = sqrt((2 * h) / g)
t = sqrt((2 * 0.790 m) / 9.8 m/s^2)
t = 0.4 s (rounded to one decimal place)
Horizontal distance covered by the block:
Horizontal distance = v_block * t
Horizontal distance = 0.74495 m/s * 0.4 s
Horizontal distance ≈ 0.298 m
Therefore, the block covers approximately 0.298 meters horizontally before hitting the ground.
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Dolphins rely on echolocation to be able to survive in the ocean. In a 20 °C ocean, a dolphin produces an ultrasonic sound with a
frequency of 125 kHz. Use 1530 m/s for the speed of sound in 20 °C ocean water.
What is the wavelength lambda of this sound, in meters?
The wavelength (λ) of the sound produced by the dolphin is approximately 12.24 meters.
The term "wavelength" describes the separation between two waves' successive points that are in phase, or at the same place in their respective cycles. The distance between two similar locations on a wave, such as the distance between two crests or two troughs, is what it is, in other words.
The wavelength (λ) of a sound wave can be calculated using the formula:
λ = v / f
where:
λ = wavelength of the sound wave
v = speed of sound in the medium
f = frequency of the sound wave
The speed of sound in this situation is reported as 1530 m/s in 20 °C ocean water, and the frequency of the dolphin's ultrasonic sound is 125 kHz (which may be converted to 125,000 Hz).
Substituting these values into the formula, we get:
λ = 1530 m/s / 125,000 Hz
To simplify the calculation, we can convert the frequency to kHz by dividing it by 1,000:
λ = 1530 m/s / 125 kHz
Now, let's calculate the wavelength:
λ = 1530 / 125 = 12.24 meters
Therefore, the wavelength (λ) of the sound produced by the dolphin is approximately 12.24 meters.
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Assume that your car requires a full tank of gas (15 gallons) to go on a trip to Kentucky from Columbus. A gallon of gas costs $4.15, and the car wastes 11 gallons of gas. If the engine consumes all of the gas in the gas tank how much money will you lose on gas by the time you get to Kentucky?
You would lose $16.60 on gas by the time you get to Kentucky.
To calculate the total cost of gas for the trip to Kentucky, we can follow these steps:
1. Determine the amount of gas used for the trip by subtracting the wasted gas from the full tank capacity:
Amount of gas used = Full tank capacity - Wasted gas
= 15 gallons - 11 gallons
= 4 gallons
2. Calculate the total cost of gas by multiplying the amount of gas used by the cost per gallon:
Total cost of gas = Amount of gas used × Cost per gallon
= 4 gallons × $4.15/gallon
= $16.60
Therefore, you would lose $16.60 on gas by the time you get to Kentucky.
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Mark has helium pants that allow him to float . Mark will float in the air if the buoyant force pushing him upward is greater than his weight pulling him downward. Let's assume the mark has a mass of 100 kg and has the same density as water.
1a. what is marks weight?
2a. what is the buoyant force on Mark when he is not wearing the helium pants?
3a. How much minimum volume of helium needs to be in Marks pants for him to float?
4a. If you model Mark and he's healing pens as a cube, what would be the minimum length of the side of the cube for him to float?
The minimum length of the side of the cube required for Mark to float is 9.87 meters.
1. Mark's weight is calculated as the product of his mass and the acceleration due to gravity, which is equal to 9.81m/s².
Therefore,Mark's weight = mass × acceleration due to gravity
= 100 kg × 9.81m/s²= 981 N2.
Buoyant force on Mark when he is not wearing helium pantsWhen Mark is not wearing helium pants, the buoyant force acting on him is equal to the weight of the water displaced by his body. Mark's body displaces a volume of water equal to his own volume, and since he has the same density as water, his weight is equal to the weight of the water he displaces, which is given by:
Weight of water displaced = Density of water × Volume of water displaced
= 1000 kg/m³ × 100 kg'
= 100,000 N
Therefore, the buoyant force acting on Mark when he is not wearing helium pants is 100,000 N.3. Minimum volume of helium required for Mark to float For Mark to float, the buoyant force acting on him must be greater than or equal to his weight. Therefore, the minimum buoyant force required to lift Mark is 981 N. Since helium is less dense than air, it creates a buoyant force when enclosed in a sealed container such as Mark's pants.
Therefore, the minimum volume of helium required to create a buoyant force of 981 N is given by:
Buoyant force = Weight of helium displacedDensity of air × g × Volume of helium
Volume of helium = Buoyant force × Density of air × gWeight of helium displaced
= 981 N× 1.2 kg/m³× 9.81 m/s²
= 11,501.28 N
The minimum volume of helium required for Mark to float is:
Volume of helium = 11,501.28 N / (1.2 kg/m³ × 9.81 m/s²)
= 966.32 m³.4. Minimum length of the cubeMark's pants can be modeled as a cube. The minimum length of the side of the cube required to hold 966.32 m³ of helium can be calculated using the formula for the volume of a cube, which is given by:
Volume of cube = Length³
Length³ = Volume of cube
Length = [tex](Volume of cube)^_(1/3)[/tex]
= [tex](966.32 m³)^_(1/3)[/tex]
= 9.87 m
Therefore, the minimum length of the side of the cube required for Mark to float is 9.87 meters.
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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
The ratio of the voltage in the secondary coil to the voltage in the primary coil is approximately 1,290.3.
The ratio of the voltage in the secondary coil to the voltage in the primary coil (Vsecondary/Vprimary) can be calculated using the formula:
Nsecondary/Nprimary = Vsecondary/Vprimary
Given that Nprimary = 10 and Nsecondary = 12,903, we can substitute these values into the formula:
12,903/10 = Vsecondary/Vprimary
Simplifying the equation, we find:
Vsecondary/Vprimary = 1,290.3
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12. (1 p) Consider two different media, one water and the other unknown. With them, the critical angle is determined to be 550 What is the refractive index of this unknown medium?
The refractive index of an unknown medium, using the critical angle of 550, is 1.53.
This can be determined using Snell's law which states that the ratio of the sine of the angle of incidence to the sine of the angle of refraction is equal to the refractive index of the medium. The critical angle is the angle of incidence that results in an angle of refraction of 90°. When the angle of incidence is greater than the critical angle, the light undergoes total internal reflection, meaning that it does not leave the medium but is reflected back into it.
In this question, we are given two different media, water and an unknown medium. We are also given the critical angle for these media, which is 55°.
Using Snell's law, we can write: n1 sin θ1 = n2 sin θ2
where n1 is the refractive index of water, θ1 is the angle of incidence in water, n2 is the refractive index of the unknown medium, and θ2 is the angle of refraction in the unknown medium.
At the critical angle, θ2 = 90°.
Therefore, we can write:
n1 sin θ1 = n2 sin 90°n1 sin θ1 = n2
We know that the refractive index of water is approximately 1.33.
Substituting this value into the equation above, we get:
1.33 sin 55° = n2sin 55°
= n2/1.33
n2 = sin 55° × 1.33
n2 = 1.53
Therefore, the refractive index of the unknown medium is approximately 1.53.
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