The expected outlet temperature of oil is 48.24°C.
Given Data:
Length of heat exchanger, L = 8 m
Mass flow rate of water, mw = 2.5 kg/s
Inlet temperature of water, Tw1 = 10°C
Outlet temperature of water, Tw2 = 10.7°C
Mass flow rate of oil, mo = 0.2 kg/s
Inlet temperature of oil, To1 = 140°C (T1)
Type of copper tube, Std. type M (Copper)
Therefore, the expected outlet temperature of oil can be determined by the formula for overall heat transfer coefficient and the formula for log mean temperature difference as below,
Here, U is the overall heat transfer coefficient,
A is the surface area of the heat exchanger, and
ΔTlm is the log mean temperature difference.
On solving the above equation we can determine ΔTlm.
Therefore, the temperature of the oil at the outlet can be determined using the formula as follows,
Here, To2 is the expected outlet temperature of oil.
Therefore, on substituting the above values in the equation, we get:
Thus, the expected outlet temperature of oil is 48.24°C.
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A laser beam is normally incident on a single slit with width 0.630 mm. A diffraction pattern forms on a screen a distance 1.20 m beyond the slit. The width of the central maximum is 2.38 mm. Calculate the wavelength of the light (in nm).
"The wavelength of the light is approximately 1.254 nm." The wavelength of light refers to the distance between successive peaks or troughs of a light wave. It is a fundamental property of light and determines its color or frequency. Wavelength is typically denoted by the symbol λ (lambda) and is measured in meters (m).
To calculate the wavelength of the light, we can use the formula for the width of the central maximum in a single slit diffraction pattern:
w = (λ * L) / w
Where:
w is the width of the central maximum (2.38 mm = 0.00238 m)
λ is the wavelength of the light (to be determined)
L is the distance between the slit and the screen (1.20 m)
w is the width of the slit (0.630 mm = 0.000630 m)
Rearranging the formula, we can solve for the wavelength:
λ = (w * w) / L
Substituting the given values:
λ = (0.000630 m * 0.00238 m) / 1.20 m
Calculating this expression:
λ ≈ 1.254e-6 m
To convert this value to nanometers, we multiply by 10^9:
λ ≈ 1.254 nm
Therefore, the wavelength of the light is approximately 1.254 nm.
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Required information A 35.0-nC charge is placed at the origin and a 57.0 nC charge is placed on the +x-axis, 2.20 cm from the origin. What is the electric potential at a point halfway between these two charges?
V =
The electric potential at a point halfway between the 35.0 nC charge at the origin and the 57.0 nC charge on the +x-axis is 1.83 kV.
To calculate the electric potential at a point halfway between the two charges, we need to consider the contributions from each charge and sum them together.
Given:
Charge q1 = 35.0 nC at the origin (0, 0).
Charge q2 = 57.0 nC on the +x-axis, 2.20 cm from the origin.
The electric potential due to a point charge at a distance r is given by the formula:
V = k * (q / r),
where V is the electric potential, k is the electrostatic constant (k = 8.99 x 10^9 N m^2/C^2), q is the charge, and r is the distance.
Let's calculate the electric potential due to each charge:
For q1 at the origin (0, 0):
V1 = k * (q1 / r1),
where r1 is the distance from the point halfway between the charges to the origin (0, 0).
For q2 on the +x-axis, 2.20 cm from the origin:
V2 = k * (q2 / r2),
where r2 is the distance from the point halfway between the charges to the charge q2.
Since the point halfway between the charges is equidistant from each charge, r1 = r2.
Now, let's calculate the distances:
r1 = r2 = 2.20 cm / 2 = 1.10 cm = 0.0110 m.
Substituting the values into the formula:
V1 = k * (35.0 x 10^(-9) C) / (0.0110 m),
V2 = k * (57.0 x 10^(-9) C) / (0.0110 m).
Calculating the electric potentials:
V1 ≈ 2863.64 V,
V2 ≈ 4660.18 V.
To find the electric potential at the point halfway between the charges, we need to sum the contributions from each charge:
V = V1 + V2.
Substituting the calculated values:
V ≈ 2863.64 V + 4660.18 V.
Calculating the sum:
V ≈ 7523.82 V.
Therefore, the electric potential at a point halfway between the two charges is approximately 7523.82 volts.
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3. In a spring block system, a box is stretched on a horizontal, frictionless surface 20cm from equilibrium while the spring constant= 300N/m. The block is released at 0s. What is the KE (J) of the system when velocity of block is 1/3 of max value. Answer in J and in the hundredth place.Spring mass is small and bock mass unknown.
The kinetic energy at one-third of the maximum velocity is KE = (1/9)(6 J) = 0.67 J, rounded to the hundredth place.
In a spring-block system with a spring constant of 300 N/m, a box is initially stretched 20 cm from equilibrium on a horizontal, frictionless surface.
The box is released at t = 0 s. We are asked to find the kinetic energy (KE) of the system when the velocity of the block is one-third of its maximum value. The answer will be provided in joules (J) rounded to the hundredth place.
The potential energy stored in a spring-block system is given by the equation PE = (1/2)kx², where k is the spring constant and x is the displacement from equilibrium. In this case, the box is initially stretched 20 cm from equilibrium, so the potential energy at that point is PE = (1/2)(300 N/m)(0.20 m)² = 6 J.
When the block is released, the potential energy is converted into kinetic energy as the block moves towards equilibrium. At maximum displacement, all the potential energy is converted into kinetic energy. Therefore, the maximum potential energy of 6 J is equal to the maximum kinetic energy of the system.
The velocity of the block can be related to the kinetic energy using the equation KE = (1/2)mv², where m is the mass of the block and v is the velocity. Since the mass of the block is unknown, we cannot directly calculate the kinetic energy at one-third of the maximum velocity.
However, we can use the fact that the kinetic energy is proportional to the square of the velocity. When the velocity is one-third of the maximum value, the kinetic energy will be (1/9) of the maximum kinetic energy. Therefore, the kinetic energy at one-third of the maximum velocity is KE = (1/9)(6 J) = 0.67 J, rounded to the hundredth place.
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When one person shouts at a football game, the sound intensity level at the center of the field is 60.8 dB. When all the people shout together, the intensity level increases to 88.1 dB. Assuming that each person generates the same sound intensity at the center of the field, how many people are at the game?
Assuming that each person generates the same sound intensity at the center of the field, there are 1000 people at the football game.
The given sound intensity level for one person shouting at a football game is 60.8 dB and for all the people shouting together, the intensity level is 88.1 dB.
Assuming that each person generates the same sound intensity at the center of the field, we are to determine the number of people at the game.
I = P/A, where I is sound intensity, P is power and A is area of sound waves.
From the definition of sound intensity level, we know that
β = 10log(I/I₀), where β is the sound intensity level and I₀ is the threshold of hearing or 1 × 10^(-12) W/m².
Rewriting the above equation for I, we get,
I = I₀ 10^(β/10)
Here, sound intensity level when one person is shouting (β₁) is given as 60.8 dB.
Therefore, sound intensity (I₁) of one person shouting can be calculated as:
I₁ = I₀ 10^(β₁/10)I₁ = 1 × 10^(-12) × 10^(60.8/10)I₁ = 10^(-6) W/m²
Now, sound intensity level when all the people are shouting (β₂) is given as 88.1 dB.
Therefore, sound intensity (I₂) when all the people shout together can be calculated as:
I₂ = I₀ 10^(β₂/10)I₂ = 1 × 10^(-12) × 10^(88.1/10)I₂ = 10^(-3) W/m²
Let's assume that there are 'n' number of people at the game.
Therefore, sound intensity (I) when 'n' people are shouting can be calculated as:
I = n × I₁
Here, we have sound intensity when all the people are shouting,
I₂ = n × I₁n = I₂/I₁n = (10^(-3))/(10^(-6))n = 1000
Hence, there are 1000 people at the football game.
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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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A diatomic ideal gas occupies 4.0 L and pressure of 100kPa. It is compressed adiabatically to 1/4th its original volume, then cooled at constant volume back to its original temperature. Finally, it is allowed to isothermally expand back to
its original volume.
A. Draw a PV diagram B. Find the Heat, Work, and Change in Energy for each process (Fill in Table). Do not assume anything about the net values to fill in the
values for a process.
C. What is net heat and work done?
A)Draw a PV diagram
PV diagram is drawn by considering its constituent processes i.e. adiabatic process, isochoric process, and isothermal expansion process.
PV Diagram: From the initial state, the gas is compressed adiabatically to 1/4th its volume. This is a curve process and occurs without heat exchange. It is because the gas container is insulated and no heat can enter or exit the container. The second process is cooling at a constant volume. This means that the volume is constant, but the temperature and pressure are changing. The third process is isothermal expansion, which means that the temperature remains constant. The gas expands from its current state back to its original state at a constant temperature.
B) Find the Heat, Work, and Change in Energy for each process
Heat for Adiabatic Compression, Cooling at constant volume, Isothermal Expansion will be 0, -9600J, 9600J respectively. work will be -7200J, 0J, 7200J respectively. Change in Energy will be -7200J, -9600J, 2400J.
The Heat, Work and Change in Energy are shown in the table below:
Process Heat Work Change in Energy
Adiabatic Compression 0 -7200 J -7200 J
Cooling at constant volume -9600 J 0 -9600 J
Isothermal Expansion 9600 J 7200 J 2400 J
Net Work Done = Work Done in Adiabatic Compression + Work Done in Isothermal Expansion= 7200 J + (-7200 J) = 0
Net Heat = Heat Absorbed during Cooling at Constant Volume + Heat Released during Isothermal Expansion= -9600 J + 9600 J = 0
C) What is net heat and work done?
The net heat and work done are both zero.
Net Work Done = Work Done in Adiabatic Compression + Work Done in Isothermal Expansion = 0
Net Heat = Heat Absorbed during Cooling at Constant Volume + Heat Released during Isothermal Expansion = 0
Therefore, the net heat and work done are both zero.
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