The minimum amount of force needed to get the block moving is 19.4 N.
mass of block m= 5.5 kg
The slope of the ramp θ = 35°
The coefficient of static friction μs= 0.60
The coefficient of kinetic friction μk= 0.44
The force required to move the block is called the force of friction. If the force is large enough to move the block, then the force of friction equals the force of the push. If the force of the push is less than the force of friction, then the block will not move.
A force diagram can be drawn to determine the frictional force acting on the block.The gravitational force acting on the block can be broken down into two components, perpendicular and parallel to the ramp.The frictional force is acting up the ramp, opposing the force parallel to the ramp applied to the block.
To find the minimum amount of force needed to get the block moving, we have to consider the maximum frictional force. This maximum force of static friction is defined as
`μs * N`.
Where
`N = m * g` is the normal force acting perpendicular to the plane.
In general, the frictional force acting on an object is given by the following formula:
Frictional force, F = μ * N
Where
μ is the coefficient of friction
N is the normal force acting perpendicular to the plane
We have to consider the maximum static frictional force which is
`μs * N`.
To find the normal force, we need to find the component of gravitational force acting perpendicular to the ramp:
mg = m * g = 5.5 * 9.8 = 53.9 N
component of gravitational force parallel to ramp = m * g * sin θ = 53.9 * sin 35 = 30.97 N
component of gravitational force perpendicular to ramp = m * g * cos θ = 53.9 * cos 35 = 44.1 N
For an object on an incline plane, the normal force is equal to the component of gravitational force perpendicular to the ramp.
Thus, N = 44.1 N
maximum force of static friction = μs * N = 0.6 * 44.1 = 26.5 N
Now that we know the maximum force of static friction, we can determine the minimum force required to move the block.
The minimum force required to move the block is equal to the force of kinetic friction, which is defined as `μk * N`.
minimum force required to move the block = μk * N = 0.44 * 44.1 = 19.4 N
Therefore, the minimum amount of force needed to get the block moving is 19.4 N.
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In a particular application, the current in the inner conductor is 1.30 A out of the page, and the current in the outer conductor is 2.52 A into the page. Determine the magnitude of the magnetic field at point Tries 0/10 Determine the magnitude of the magnetic field at point b. Tries 0/10
Therefore, the magnitude of the magnetic field at point T due to the inner conductor is 5.49 x 10^-6 Tesla, and the magnitude of the magnetic field at point T due to the outer conductor is 1.94 x 10^-6 Tesla. Note that the direction of the magnetic field is out of the page for the inner conductor and into the page for the outer conductor.
Given the following information:Current flowing through inner conductor = 1.30 A (out of the page)Current flowing through outer conductor = 2.52 A (into the page)To determine the magnitude of the magnetic field at point T, we use the right-hand thumb rule, which states that if we grip a wire with our right hand and point our thumb in the direction of current flow, our fingers will curl in the direction of the magnetic field (i.e. counter-clockwise or clockwise).
Since the current is out of the page in the inner conductor, the magnetic field is also directed out of the page. For the outer conductor, the current is flowing into the page, so the magnetic field is directed into the page.Using Ampere's circuital law, we can find the magnitude of the magnetic field at point T.
Ampere's law states that the line integral of the magnetic field around a closed path is equal to the current enclosed by the path times the permeability of free space (μ0).B = μ0I / 2πrWhere,I = Current enclosed by the pathμ0 = Permeability of free space = 4π x 10^-7 Tesla meter per ampere2πr = Circumference of the circular path at point TFor the inner conductor, the current enclosed by the path is 1.30 A, soB = (4π x 10^-7) x 1.30 / (2π x 0.15) = 5.49 x 10^-6 Tesla
For the outer conductor, the current enclosed by the path is 2.52 A - 1.30 A = 1.22 A, soB = (4π x 10^-7) x 1.22 / (2π x 0.25) = 1.94 x 10^-6 Tesla
Therefore, the magnitude of the magnetic field at point T due to the inner conductor is 5.49 x 10^-6 Tesla, and the magnitude of the magnetic field at point T due to the outer conductor is 1.94 x 10^-6 Tesla. Note that the direction of the magnetic field is out of the page for the inner conductor and into the page for the outer conductor.
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Most nuclear reactors contain many critical masses. Why do they not go supercritical? What are two methods used to control the fission in the reactor?
Nuclear reactors have many critical masses, but they do not go supercritical because of the control rods and water.
Nuclear reactors are large and complex systems of machinery that produce heat, which is then converted into electricity. A nuclear reactor is an example of nuclear technology in action. Nuclear technology is the application of nuclear science in various fields like energy production, medicine, and many others.
To understand this, it is important to understand what is meant by the term critical mass in the context of nuclear reactors.
Critical mass refers to the amount of fissile material required to maintain a chain reaction. It's the point at which a reaction becomes self-sustaining. The chain reaction results in the release of a tremendous amount of energy, as well as the creation of new particles and isotopes that are radioactive.
There are two ways to control the fission in the reactor, which are as follows:
Control rods: Control rods are made of neutron-absorbing material, such as boron, and are inserted into the core to control the rate of the chain reaction. The rods are positioned above the fuel rods in the reactor, and their insertion or removal determines the level of reaction in the core. When the rods are fully inserted, the reaction is halted completely.
Water: Water is used in most reactors to cool the fuel rods and remove heat from the core. Water also acts as a moderator, slowing down neutrons and increasing their chances of interacting with fuel atoms. Water's ability to act as both a coolant and a moderator makes it an important part of reactor design.
In conclusion, nuclear reactors have many critical masses, but they do not go supercritical because of the control rods and water.
The control rods are made of neutron-absorbing material, and they are used to control the rate of the chain reaction. Water is used as a moderator, which slows down neutrons and increases their chances of interacting with fuel atoms.
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Figure 1 Two opposing speakers are shown in Figure 1. A standing wave is produced from two sound waves traveling in opposite directions; each can be described as follows: y 1
=(5 cm)sin(4x−2t),
y 2
=(5 cm)sin(4x+2t)
where x and y, are in centimeters and t is in seconds. Find i. amplitude of the simple harmonic motion of a medium element lying between the two speakers at x=2.5 cm. ii. amplitude of the nodes and antinodes. iii. maximum amplitude of an element at an antinode
The amplitude of the simple harmonic motion of a medium element lying between the two speakers at x=2.5 cm is 0. Ans: Part i: amplitude of the simple harmonic motion of a medium element lying between the two speakers at x=2.5 cm.
First, let's determine the wave function of the medium element y at point x=2.5 cm. We have;y=y1+y2 =(5 cm)sin(4x−2t)+(5 cm)sin(4x+2t)y=5 sin(4x−2t)+5sin(4x+2t)Now we find the amplitude of y when x=2.5 cm.
We have;y=5 sin(4(2.5)−2t)+5sin(4(2.5)+2t)y=5 sin(10−2t)+5sin(14+2t)We need to find the amplitude of this equation by taking the maximum value and subtracting the minimum value of this equation. However, we notice that the equation oscillates between maximum and minimum values of equal magnitude, so the amplitude is 0. Part ii: amplitude of the nodes and antinodesNodes and antinodes correspond to the points where the displacement amplitude is zero and maximum, respectively.
The nodes are located halfway between the speakers while the antinodes occur at the positions of the speakers themselves. Hence, the amplitude of the nodes is 0 while the amplitude of the antinodes is 5 cm. Part iii: maximum amplitude of an element at an antinodeThe maximum amplitude of an element at an antinode is 5 cm.
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Calculate the following: a) A point charge q is located at distance z above a grounded conducting plane. Find the net force exerted by the conducting plane on the charge. b) Calculate the induced charge density on the conducting plane.
The net force exerted by the conducting plane on the charge, Net force = -q² / [2ε(h+z)²].
Induced charge density on the conducting plane is, Induced charge density = -q / (2πh) where q is the charge and h is the distance of charge q from the grounded conducting plane.
a. The net force exerted on the point charge by the grounded conducting plane:
Given that a point charge q is located at a distance z above a grounded conducting plane, we want to find the net force exerted by the conducting plane on the charge.
We define h as the distance of charge q from the grounded conducting plane. The net force exerted on the point charge by the grounded conducting plane is given by the equation:
F = -q² / [2ε(h+z)²]
where ε represents the permittivity of free space. The negative sign in the expression indicates that the net force exerted by the conducting plane is opposite to the direction of the charge q.
b. The induced charge density on the conducting plane:
The induced charge density can be calculated by,
Induced charge density = -q / (2πh)
This formula provides the charge density induced on the conducting plane as a result of the presence of the point charge q, where q is the charge and h is the distance of charge q from the grounded conducting plane.
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b) Obtain Tc, the temperature at point c.
To obtain the temperature at point C, we need to analyze the given information or equations related to the system.
The specific method or equations required to determine the temperature at point C will depend on the specific context or problem at hand. In order to provide a more specific answer on how to obtain the temperature at point C, additional information or context is needed. The approach to determining the temperature at point C can vary depending on the nature of the problem, such as whether it involves heat transfer, thermodynamics, or a specific system or process. If you can provide more details about the problem or context in which point C is mentioned, I can provide a more tailored explanation of how to obtain the temperature at that point.
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Without plagiarizing. Write a meaningful Thesis paragraph about
Einstein's life and Contribution to quantum physics
Here is a Thesis about Einstein's life and Contribution to quantum physics.
Albert Einstein, widely regarded as the most brilliant scientist of the twentieth century, was one of the pioneering figures in the field of quantum physics.
He was a theoretical physicist who is best known for developing the theory of relativity and for his contributions to the development of quantum mechanics. Einstein's work in quantum physics helped to revolutionize our understanding of the nature of reality and the behavior of matter at the atomic and subatomic levels. His contributions to the field have had a profound impact on modern physics, and his ideas continue to influence research in this area to this day.
This paper will explore Einstein's life and his significant contribution to quantum physics.
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A spacecraft is moving through a vaccum. It changes its velocity from 9050 ft/sec to 5200 ft/sec in 48 seconds. Calculate the power required to accomplished this if the spacecraft mass is 13,000 slugs.
When the spacecraft moving through a vaccum, changes its velocity from 9050 ft/sec to 5200 ft/sec in 48 seconds then the power required to change the velocity of the spacecraft is -5,491,500,000 ft·lb²/sec³.
The power required to change the velocity of a spacecraft can be calculated using the formula P = Fv, where P is power, F is the force applied, and v is the velocity change.
First, we need to find the force applied to the spacecraft.
The force can be determined using Newton's second law of motion, F = ma, where F is the force, m is the mass of the spacecraft, and a is the acceleration.
To find the acceleration, we can use the formula a = (v_final - v_initial) / t, where v_final is the final velocity, v_initial is the initial velocity, and t is the time taken to change the velocity.
Given that the initial velocity (v_initial) is 9050 ft/sec, the final velocity (v_final) is 5200 ft/sec, and the time (t) is 48 seconds, we can calculate the acceleration:
a = (5200 - 9050) / 48 = -81.25 ft/sec²
Since the spacecraft is decelerating, the acceleration is negative.
Now we can calculate the force:
F = ma = 13000 slugs * -81.25 ft/sec² = -1,056,250 ft·lb/sec²
Finally, we can calculate the power:
P = Fv = (-1,056,250 ft·lb/sec²) * 5200 ft/sec = -5,491,500,000 ft·lb²/sec³
Therefore, the power required to change the velocity of the spacecraft is -5,491,500,000 ft·lb²/sec³.
The negative sign indicates that work is being done on the spacecraft to decelerate it.
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A 200 g metal container, insulated on the outside, holds 100 g of water in thermal equilibrium at 22.0°C. A 9 g ice cube, at temperature -20.0°C, is dropped into the water, and when thermal equilibrium is reached the temperature is 12.0°C. Assume there is no heat exchange with the surroundings. Find the specific heat of the metal the container is made from. cwater = 4190 J/kg∙C°
cice = 2090 J/kg∙C°
Lf = 3.34×105 J/kg
The specific heat of the metal container is approximately 2095 J/kg∙C°.
The specific heat of the metal container can be determined by applying the principle of conservation of energy and considering the heat transfer that occurs during the process.
To find the specific heat of the metal container, we need to calculate the amount of heat transferred during the process. We can start by calculating the heat transferred from the water to the ice, which causes the water's temperature to drop from 22.0°C to 12.0°C.
The heat transferred from the water to the ice can be calculated using the formula:
Qwater → ice = mcΔT
where:
m is the mass of the water (100 g),
c is the specific heat of water (4190 J/kg∙C°), and
ΔT is the change in temperature (22.0°C - 12.0°C = 10.0°C).
Substituting the given values into the equation, we have:
Qwater → ice = (0.1 kg) * (4190 J/kg∙C°) * (10.0°C) = 4190 J
The heat transferred from the water to the ice is equal to the heat gained by the ice, causing it to melt. The heat required to melt the ice can be calculated using the formula:
Qmelting = mLf
where:
m is the mass of the ice (9 g),
Lf is the latent heat of fusion for ice (3.34×10^5 J/kg).
Substituting the given values into the equation, we have:
Qmelting = (0.009 kg) * (3.34×10^5 J/kg) = 3010 J
Since the metal container is insulated and there is no heat exchange with the surroundings, the heat transferred from the water to the ice and the heat required to melt the ice must be equal. Therefore, we can equate the two equations:
Qwater → ice = Qmelting
4190 J = 3010 J
Now, we can solve for the specific heat of the metal container (cm) by rearranging the equation:
cm = Qwater → ice / (mwater * ΔTwater)
Substituting the known values, we get:
cm = (4190 J) / ((0.2 kg) * (10.0°C)) ≈ 2095 J/kg∙C°
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Find the electric potential induced by an uniformly polarized sphere (radius R, R polarization P). (15 marks)
The electric potential induced by a uniformly polarized sphere with radius R and polarization P is given by the formula V = (1/4πε₀) * (P/R).
The electric potential induced by a uniformly polarized sphere can be calculated using the formula V = (1/4πε₀) * (P/R).
The polarization of a sphere is a measure of the dipole moment per unit volume. It indicates the extent to which the charges in the sphere are displaced from their equilibrium positions. When a sphere is uniformly polarized, the dipole moment is constant throughout the volume of the sphere.
By using this formula, you can calculate the electric potential induced by a uniformly polarized sphere for a given radius and polarization. This provides a useful tool for understanding the electrical behavior of polarized spheres and their impact on the surrounding electric field.
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A proton moving perpendicular to a magnetic field of 9.80 μT follows a circular path of radius 4.95 cm. What is the proton's speed? Please give answer in m/s. 2.) If the magnetic field in the previous question is pointed into the page and the proton is moving to the left when it enters the region of the magnetic field, the proton goes in what direction as viewed from above? Group of answer choices a) Clockwise b.) Counterclockwise c.) Down the page d.) Up the page
The proton's speed is 4.71 × 10⁵ m/s. 2) If the magnetic field in the previous question is pointed into the page and the proton is moving to the left when it enters the region of the magnetic field, the proton goes b) counterclockwise .
A proton moves perpendicular to a magnetic field of 9.80 μT follows a circular path of radius 4.95 cm.
To find the proton's speed, we can use the formula:
magnetic force = centripetal force
qvB = (mv²)/r
where q is the charge of the proton v is the velocity of the proton m is the mass of the proton B is the magnetic field r is the radius of the circular path
v = r Bq/m
Substitute the given values:
r = 4.95 cm = 0.0495 mB = 9.80 μT = 9.80 × 10⁻⁶ TMp = 1.67 × 10⁻²⁷ kgq = 1.60 × 10⁻¹⁹ Cv = (0.0495 m)(9.80 × 10⁻⁶ T)(1.60 × 10⁻¹⁹ C)/(1.67 × 10⁻²⁷ kg)v = 4.71 × 10⁵ m/s
Therefore, the proton's speed is 4.71 × 10⁵ m/s.
2. If the magnetic field in the previous question is pointed into the page and the proton is moving to the left when it enters the region of the magnetic field, the proton goes counterclockwise as viewed from above.
Answer: b) Counterclockwise.
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If a runners power is 400 W as runs, how much chemical energy does she convert into other forms in 10.0 minutes?
Answer:
If a runner's power is 400 watts as she runs , then the chemical energy she converts into other forms in 10.0 minutes would be 240,000 Joules . This information may be found in several of the search results provided, including result numbers 1, 2, 4, 5, 6, 8, and 9.
Explanation:
A rocket is launched from the Rocket Lab launch site at Mahia (latitude 39 south). Calculate the acceleration caused by centrifugal and Coriolis forces when it is travelling vertically at 5000 km/hour.
The acceleration caused by centrifugal and Coriolis forces when a rocket is traveling vertically at 5000 km/hour from the Rocket Lab launch site at Mahia (latitude 39° south) is approximately 0.079 m/s².
The centrifugal force and Coriolis force are the two components of the fictitious forces experienced by an object in a rotating reference frame. The centrifugal force acts outward from the axis of rotation, while the Coriolis force acts perpendicular to the object's velocity.
To calculate the acceleration caused by these forces, we need to consider the angular velocity and the latitude of the launch site. The angular velocity [tex](\( \omega \))[/tex] can be calculated using the rotational period of the Earth T:
[tex]\[ \omega = \frac{2\pi}{T} \][/tex]
The centrifugal acceleration [tex](\( a_c \))[/tex]can be calculated using the formula:
[tex]\[ a_c = \omega^2 \cdot R \][/tex]
where R is the distance from the axis of rotation (in this case, the radius of the Earth).
The Coriolis acceleration[tex](\( a_{\text{cor}} \))[/tex] can be calculated using the formula:
[tex]\[ a_{\text{cor}} = 2 \cdot \omega \cdot v \][/tex]
where v is the velocity of the rocket.
Given that the latitude is 39° south, we can determine the radius of the Earth R at that latitude using the formula:
[tex]\[ R = R_{\text{equator}} \cdot \cos(\text{latitude}) \][/tex]
Substituting the given values and performing the calculations, we find that the acceleration caused by centrifugal and Coriolis forces is approximately 0.079 m/s².
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All or dont answer
After an electron is accelerated from rest through a potential difference, it has a de Broglie wavelength of 645 nm. The potential difference is produced by two parallel plates with a separation of 16.5 mm. ( gravity and relativistic effects can be ignored)
1. What is the final velocity of the electron?
2.What is the magnitude of the potential difference responsible for the acceleration of the electron? in μV
3. What is the magnitude of the electric field between the plates? in mV/m.
1. The velocity (v) of the electron to be approximately 2.4 × 10^6 m/s.
2. The acceleration of the electron is approximately 1300 V.
3. The magnitude of the electric field between the plates is approximately 78.8 mV/m.
To solve the problem, we can use the de Broglie wavelength equation and the equations for potential difference and electric field.
1. The de Broglie wavelength (λ) of a particle can be related to its velocity (v) by the equation:
λ = h / (mv)
Where h is the Planck's constant and m is the mass of the particle.
Given λ = 645 nm (convert to meters: 645 × 10^-9 m)
Assuming the electron mass (m) is 9.11 × 10^-31 kg
Planck's constant (h) is 6.626 × 10^-34 J·s
We can rearrange the equation to solve for the velocity:
v = h / (mλ)
Substituting the values:
v = (6.626 × 10^-34 J·s) / ((9.11 × 10^-31 kg)(645 × 10^-9 m))
2. The potential difference (V) between the parallel plates can be related to the kinetic energy (K) of the electron by the equation:
K = eV
Where e is the elementary charge (1.6 × 10^-19 C).
To find the potential difference, we need to find the kinetic energy of the electron. The kinetic energy can be related to the velocity by the equation:
K = (1/2)mv^2
Substituting the values:
K = (1/2)(9.11 × 10^-31 kg)(2.4 × 10^6 m/s)^2
Using a calculator, we find the kinetic energy (K) of the electron.
Finally, we can find the potential difference (V):
V = K / e
Substituting the calculated kinetic energy and the elementary charge:
V = (1/2)(9.11 × 10^-31 kg)(2.4 × 10^6 m/s)^2 / (1.6 × 10^-19 C) = 1300 V.
3. The electric field (E) between the plates can be calculated using the potential difference (V) and the distance between the plates (d) by the equation:
E = V / d
Substituting the calculated potential difference and the distance between the plates:
E = 1300 V / (16.5 × 10^-3 m) = 78.8 mV/m.
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At the last stage of stellar evolution, a heavy star can collapse into an extremely dense object made mostly of neutrons. The star is called a neutron star. Suppose we represent the star as a uniform, solid, rigid sphere, both before and after the collapse. The star's initial radius was the solar radius 8.5×10 5
km; its final radius is 7.1 km. If the original star rotated with the solar rotation period 19 days, find the rotation period of the collapsed neutron star in the unit of millisecond.
At the last stage of stellar evolution, a heavy star can collapse into an extremely dense object made mostly of neutrons. the rotation period of the collapsed neutron star is approximately 0.5 milliseconds.
To find the rotation period of the collapsed neutron star, we can apply the principle of conservation of angular momentum. Since the neutron star is a rigid object, its angular momentum will remain constant before and after the collapse.
The formula for angular momentum (L) is given by the product of moment of inertia (I) and angular velocity (ω):
L = I * ω
Since the neutron star is assumed to be a uniform, solid, rigid sphere, its moment of inertia can be calculated using the formula for a solid sphere:
I = (2/5) * M * R²
Where M is the mass of the neutron star and R is its radius.
Now, let's consider the initial star and the collapsed neutron star:
For the initial star:
Initial radius (R_initial) = 8.5 × 10^5 km
Initial rotation period (T_initial) = 19 days
For the neutron star:
Final radius (R_final) = 7.1 km
Final rotation period (T_final) = unknown (to be calculated)
The mass (M) of the star remains the same before and after the collapse.
Using the conservation of angular momentum, we can equate the initial and final angular momenta:
I_initial * ω_initial = I_final * ω_final
Substituting the expressions for moment of inertia and angular velocity:
[(2/5) * M * R_initial²] * (2π / T_initial) = [(2/5) * M * R_final²] * (2π / T_final)
Simplifying the equation and canceling common factors:
(R_initial² / T_initial) = (R_final² / T_final)
Substituting the known values:
[(8.5 × 10^5 km)² / (19 days)] = [(7.1 km)² / T_final]
Converting the units to a common form:
[(8.5 × 10^5 km)² / (19 days)] = [(7.1 km)² / (T_final * 86,400 seconds/day)]
Solving for T_final:
T_final = [(7.1 km)² * (19 days) * (86,400 seconds/day)] / [(8.5 × 10^5 km)²]
Calculating the value:
T_final ≈ 0.5 milliseconds
Therefore, the rotation period of the collapsed neutron star is approximately 0.5 milliseconds.
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The work function of a metal surface is 4.80 x 10⁻¹⁹ J. The maximum speed of the emitted electrons is va = 730 km/s when the wavelength of the light is λA. However, a maximum speed of vB = 500 km/s is observed when the wavelength is λB. Find the wavelengths.
The wavelengths of the electrons at maximum speed 730km/s and 500 km/s are 1.008 × 10^-12 km and 6.9× 10^-13 km respectively.
What is wavelength?Wavelength is the distance between identical points (adjacent crests) in the adjacent cycles of a waveform signal propagated in space or along a wire.
Wavelength can also be defined as the distance between two successive crest or trough.
Work function of a surface is the minimum energy required to a free electrons to come out of the metal surface.
W = h( v/λ)
where h is the Planck constant = 6.63 × 10^-34 J/s
Therefore;
4.80 × 10^-19 = 6.63 × 10^-34 × 730/λ
λ = 6.63 × 10^-34 × 730)/4.80 × 10^-19
λ = 1.008 × 10^-12 km
Also
4.80 × 10^-19 = 6.63 × 10^-34 × 500/λ
λ = 6.63 × 10^-34 × 500)/4.80 × 10^-19
λ = 6.9× 10^-13 km
Therefore the wavelengths are 1.008 × 10^-12 km and 6.9× 10^-13 km
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Long, straight conductors with square cross section, each carrying current 1.2 amps, are laid side by side to form an infinite current sheet with current directed out of the plane of the page. A second infinite current sheet is a distance 3.6 cm below the first and is parallel to it. The second sheet carries current into the plane of the page. Each sheet has 200 conductors per cm. Calculate the magnitude of the net magnetic field midway between the two sheets.
The magnitude of the net magnetic field midway between the two sheets is zero for the given electric currentb
The formula for calculating the magnetic field at a point due to a current element is given by the Biot-Savart law.Using Biot-Savart's law, the magnitude of the magnetic field at a point midway between two infinite current sheets is given by;[tex]$$B=\frac{\mu_0}{4\pi}\left( \frac{I_1}{y} + \frac{I_2}{y}\right)$$[/tex]
where; μ0 is the magnetic constant or permeability of free space, I1 is the current carried by the first sheet, I2 is the current carried by the second sheet, and y is the distance between the two sheets, which is 3.6 cm.The number of conductors per unit length is given as 200.
The total current carried by each sheet is given by multiplying the current in each conductor by the number of conductors per unit length, then multiplying that product by the width of the sheet.$$I = 200 \times I_c \times w$$where;Ic = current per conductor = 1.2 Aand w = width of the sheet.The width of each conductor, a = side of the square cross-section = 1 cm.The width of each sheet, b = 200a = 200 cm
The total current carried by the first sheet, I1 = 200 × 1.2 × 200 = 48,000 A
The total current carried by the second sheet, I2 = 200 × 1.2 × 200 = 48,000 A
Therefore, the net magnetic field midway between the two sheets is given by;[tex]$$B=\frac{\mu_0}{4\pi}\left( \frac{I_1}{y} + \frac{I_2}{y}\right)$$$$B=\frac{10^{-7}}{4\pi}\left( \frac{48000}{0.036} - \frac{48000}{0.036}\right)$$$$B=\frac{10^{-7}}{4\pi} \times 0$$$$B=0$$[/tex]
The magnitude of the net magnetic field midway between the two sheets is zero.
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You have an 8 -pole DC machine with a lap winding. The emf generated by the machine is 118 V. What would the emf of a similar machine with a wave winding be?
The emf of a similar machine with a wave winding would also be 118 V.
The emf (electromotive force) generated by a DC machine depends on various factors such as the number of poles, the speed of rotation, the magnetic field strength, and the winding configuration.
In this case, we have an 8-pole DC machine with a lap winding. Lap winding is a winding configuration where each armature coil overlaps with adjacent coils in a parallel manner.
When we consider a similar machine with a wave winding, it means the winding configuration changes to a wave winding. In a wave winding, the armature coils are connected in a wave-like pattern, where each coil is connected to the adjacent coil in a series manner.
Changing the winding configuration from lap winding to wave winding does not affect the number of poles or the magnetic field strength. Therefore, the only significant difference between the two machines is the winding configuration.
Since the emf generated by a machine depends on the speed of rotation, magnetic field strength, and winding configuration, and these factors remain the same in this scenario, the emf of a similar machine with a wave winding would still be 118 V, the same as the original machine.
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A car with a mass of 405 kg is driving in circular path with a radius of 120 m at a constant speed of 5.5 m/s. What is the magnitude of the net force on the car? Round to the nearest whole number. 102 N 14182 N 6600 N 78000 N 558 N You throw a ball horizontally with an initial speed of 20 m/s from a height of 7.2 meters. How long does it take for the ball to land? Round to two decimal places. 0.55 seconds 0.39 seconds 6.53 seconds 0.15 seconds 1.20 seconds A car is initially traveling due South at 20 m/s. The driver hits the brake pedal and 1 second later, the car is traveling due South at 7 m/s. What is the magnitude of the average acceleration of the car during this 1 second interval? 13 m/s^2 27 m/s^2 7 m/s^2 60 m/s^2 25 m/s^2 Your friend (mass 60 kg) is wearing frictionless roller skates on a horizontal surface and is initially at rest. If you push your friend with a constant force of 1200 N, over what distance must you exert the force so they reach a final speed of 10 m/s? 0.25 meters 0.5 meters 1.25 meters: 2.5 meters 5 meters
1. the magnitude of the net force on the car is 558 N. Hence, the correct option is (e) 558 N.
2. it will take 1.20 seconds for the ball to land. Hence, the correct option is (e) 1.20 seconds.
3. the magnitude of the average acceleration of the car is 13 m/s². Hence, the correct option is (a) 13 m/s².
4. the distance over which the force must be exerted is 0.5 meters. Hence, the correct option is (b) 0.5 meters.
1. Calculation of the magnitude of the net force on the car:
We know that,
Formula used for the calculation of net force is:
F = m * v²/r
F = (405 kg) * (5.5 m/s)²/120 m
F = 558 N
2. Calculation of time taken by the ball to land:
Given,
V₀ = 20 m/s, h = 7.2 m, and g = 9.81 m/s². Formula used for the calculation of time taken by the ball to land is:
t = (sqrt(2h/g))
t = sqrt(2 * 7.2/9.81)
t = 1.20 s (rounded to two decimal places)
3. Calculation of the magnitude of the average acceleration of the car:
Given,
Vᵢ = 20 m/s, Vf = 7 m/s, and t = 1 s. Formula used for the calculation of the magnitude of the average acceleration of the car is:
a = (Vf - Vᵢ)/t
a = (7 - 20)/1
a = -13 m/s²
4. Calculation of the distance over which the force must be exerted:
Given,m = 60 kg, F = 1200 N, Vf = 10 m/s, and V₀ = 0 m/s. Formula used for the calculation of the distance over which the force must be exerted is:
Vf² = V₀² + 2*a*d10² = 0 + 2*(F/m)*d10² = (2400/60)*dd = 0.5 m
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8. You observe a star through a telescope.
What happens to the apparent wavelength of the star's light as it moves toward you?
a) It gets shorter.
b) It gets longer.
c) It stays the same.
9. Explain your answer.
8. The apparent
wavelength
of the star's light gets shorter when it moves towards you.
Explanation:The wavelength of light is a measure of the distance between two successive peaks (or troughs) of a wave. As an object, such as a star, moves towards an observer, the
distance
between each successive peak of light waves appears to be shortened. This causes the apparent wavelength of the star's light to decrease, resulting in what is called blue shift.In contrast, when an object such as a star is moving away from an observer, the distance between each
successive peak
of light waves appears to be lengthened, causing the apparent wavelength of the star's light to increase. This is known as redshift.9. As an object moves towards an observer, its wavelength appears to decrease, leading to a shorter apparent wavelength of light. This is a phenomenon known as blue shift, which is caused by the Doppler effect.
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The correct answer is Option a) It gets shorter. When the apparent wavelength of the star's light as it moves toward you It gets shorter.
8. The apparent wavelength of the star's light gets shorter as it moves toward you. This phenomenon is known as "Doppler effect." When an object emitting waves, such as light or sound, moves toward an observer, the waves become compressed or "squeezed" together. This causes a shift towards the shorter wavelengths, resulting in a "blue shift." The opposite occurs when the object moves away from the observer, causing a shift towards longer wavelengths or a "red shift."
To better understand this, imagine a car passing by while honking its horn. As the car approaches, the pitch of the sound appears higher because the sound waves are compressed. Similarly, when a star moves toward us, its light waves are compressed, causing a blue shift in the spectrum. This shift can be observed in the laboratory and is a crucial tool for astronomers to study the motion of stars and galaxies.
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If an AC generator is provides a voltage given by ΔV=1.20×10 2
V " sin(30πt), and the current passes thru and Inductor with value 0.500H. Calculate the following parameters:
The rms value of current in the inductor is 169.7 A.The frequency of the generator is 15 Hz.The inductive reactance of the inductor is 47.1 Ω.
Given, ΔV=1.20×10^2V sin(30πt), and L=0.500H
We know that V = L di/dt
Here, ΔV = V = 1.20×10^2V sin(30πt)
By integrating both sides, we get∫di = (1/L)∫ΔV dt
Integrating both sides with respect to time, we get:i(t) = (1/L) ∫ΔV dt
The integral of sin(30πt) will be - cos(30πt) / (30π)
Let's substitute the values:∫ΔV dt = ∫1.20×10^2 sin(30πt) dt = -cos(30πt) / (30π)
Therefore, i(t) = (1/L) (-cos(30πt) / (30π))
Now, we can calculate the following parameters:
Peak value of current, I0= (1/L) × Vmax= (1/0.5) × 120= 240 A
So, the peak value of current is 240 A.
The rms value of current is given by Irms= I0/√2= 240/√2= 169.7 A
Therefore, the rms value of current in the inductor is 169.7 A.
The given voltage equation is ΔV=1.20×10^2 V sin(30πt)
The voltage equation is given by Vmax sinωt
Here, Vmax = 1.20×10^2V and ω = 30π
The frequency of the generator is given by f = ω / (2π) = 15 Hz
Therefore, the frequency of the generator is 15 Hz.
The inductive reactance of an inductor is given by XL= 2πfL= 2 × 3.14 × 15 × 0.5= 47.1 Ω
Therefore, the inductive reactance of the inductor is 47.1 Ω.
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current of 10.0 A, determine the magnitude of the magnetic field at a point on the common axis of the coils and halfway between them. Tries 4/10 Previous Tries
Therefore, the magnitude of the magnetic field at a point on the common axis of the coils and halfway between them is 5.42 × 10⁻⁵ T.
Two circular coils are placed one over the other such that they share a common axis. The radius of the top coil is 0.120 m and it carries a current of 2.00 A. The radius of the bottom coil is 0.220 m and it carries a current of 10.0 A.
Determine the magnitude of the magnetic field at a point on the common axis of the coils and halfway between them.Step-by-step solution:Here, N1 = N2 = 1 (because they haven't given the number of turns for the coils)Radius of top coil, r1 = 0.120 m, current in the top coil, I1 = 2.00 ARadius of bottom coil, r2 = 0.220 m, current in the bottom coil, I2 = 10.0 AWe have to determine the magnitude of the magnetic field at a point on the common axis of the coils and halfway between them,
such that,B = μ0(I1 / 2r1 + I2 / 2r2)Putting the given values in the above equation, we get,B = 4π × 10⁻⁷ (2 / 2 × 0.120 + 10 / 2 × 0.220)B = 4π × 10⁻⁷ (1 / 0.12 + 5 / 0.22)B = 5.42 × 10⁻⁵ TTherefore, the magnitude of the magnetic field at a point on the common axis of the coils and halfway between them is 5.42 × 10⁻⁵ T.
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Show understanding by giving an explanation of what occurs in AC circuits when a number of waveforms combine and how and why it occurs.
There are two waveforms present in a circuit, A and B. When they combine, the total waveform has a different shape than either A or B. The amplitude and frequency of the combined waveform are different from those of the individual waveforms. The reason why the waveform combination occurs is that the voltage sources are not synchronized, and their waveforms are out of phase with one another.
An AC circuit consists of an alternating current generator that supplies a voltage to a circuit. The voltage can change over time, and its wave shape is sinusoidal. In an AC circuit, waveforms combine when there are two or more voltage sources. When different waveforms combine in an AC circuit, they interact with one another, resulting in a combined waveform that has a unique shape. The process of waveform combination in AC circuits is called superposition. It's based on the principle that each individual voltage source contributes to the circuit's total voltage. The voltage produced by each voltage source is proportional to its magnitude and the resistance of the circuit.
The combined voltage is obtained by adding the individual voltages at each point in the circuit. Suppose there are two waveforms present in a circuit, A and B. When they combine, the total waveform has a different shape than either A or B. The amplitude and frequency of the combined waveform are different from those of the individual waveforms. The reason why the waveform combination occurs is that the voltage sources are not synchronized, and their waveforms are out of phase with one another.
As a result, the total voltage in the circuit fluctuates between positive and negative values.
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During a very quick stop, a car decelerates at 6.8 m/s2. Assume the forward motion of the car corresponds to a positive direction for the rotation of the tires (and that they do not slip on the pavement).
Randomized Variablesat = 6.8 m/s2
r = 0.255 m
ω0 = 93 rad/s
Part (a) What is the angular acceleration of its tires in rad/s2, assuming they have a radius of 0.255 m and do not slip on the pavement?
Part (b) How many revolutions do the tires make before coming to rest, given their initial angular velocity is 93 rad/s ?
Part (c) How long does the car take to stop completely in seconds?
Part (d) What distance does the car travel in this time in meters?
Part (e) What was the car’s initial speed in m/s?
Part (a). the angular acceleration of the tires is 26.67 rad/s².Part (b)the tires make approximately 80.85 revolutions before coming to rest.Part (c)the car takes 3.49 seconds to stop completely.Part (d) the car travels 83.85 meters.Part (e)the initial speed of the car was 23.7 m/s.
Part (a)Angular acceleration, α can be calculated using the formula α = at/r.Substituting at = 6.8 m/s² and r = 0.255 m, we getα = 6.8/0.255α = 26.67 rad/s²Therefore, the angular acceleration of the tires is 26.67 rad/s².
Part (b)To calculate the number of revolutions the tires make before coming to rest, we can use the formulaω² - ω0² = 2αθwhere ω0 = 93 rad/s, α = 26.67 rad/s², and ω = 0 (since the tires come to rest).Substituting these values in the above equation and solving for θ, we getθ = ω² - ω0²/2αθ = (0 - (93)²)/(2(26.67))θ = 129.97 radThe number of revolutions the tires make can be calculated as follows:Number of revolutions, n = θ/2πrwhere r = 0.255 mSubstituting the values of θ and r, we getn = 129.97/(2π(0.255))n = 80.85 revTherefore, the tires make approximately 80.85 revolutions before coming to rest.
Part (c)Time taken by the car to stop, t can be calculated as follows:t = ω/αwhere ω = 93 rad/s and α = 26.67 rad/s²Substituting these values in the above equation, we gett = 3.49 sTherefore, the car takes 3.49 seconds to stop completely.
Part (d)Distance traveled by the car, s can be calculated using the formula,s = ut + 1/2 at²where u = initial velocity = final velocity, a = deceleration = -6.8 m/s² and t = 3.49 s.Substituting the values of u, a, and t in the above equation, we get,s = ut + 1/2 at²s = ut + 1/2 (-6.8)(3.49)²s = us = 83.85 mTherefore, the car travels 83.85 meters during this time.
Part (e)Initial speed of the car, u can be calculated using the formulau = ω0 ru = 93(0.255)u = 23.7 m/sTherefore, the initial speed of the car was 23.7 m/s.
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In an insulated vessel, 255 g of ice at 0°C is added to 615 g of water at 15.0°C. (Assume the latent heat of fusion of the water is 3.33 x 105 g/kg and the specific heat is 4,186 J/kg . C.) (a) What is the final temperature of the system? °C (b) How much ice remains when the system reaches equilibrium?
In an insulated vessel, 255 g of ice at 0°C is added to 615 g of water at 15.0°C. The final temperature of the system is calculated to be 4.54°C, and the amount of ice remaining at equilibrium is determined to be 89.6g.
To find the final temperature of the system, we can use the principle of conservation of energy.
The energy gained by the ice as it warms up to the final temperature is equal to the energy lost by the water as it cools down.
First, we calculate the energy gained by the ice during its phase change from solid to liquid using the latent heat of fusion formula:
Q₁ = m × [tex]L_f[/tex],
where m is the mass of ice and [tex]L_f[/tex] is the latent heat of fusion.
Substituting the given values, we find
Q₁ = (0.255 kg) × (3.33 × 10⁵ J/kg) = 84,915 J.
Next, we calculate the energy gained by the ice as it warms up from 0°C to the final temperature, using the specific heat formula:
Q₂ = m × c × ΔT,
where c is the specific heat and ΔT is the change in temperature.
Substituting the values, we find:
Q₂ = (0.255 kg) × (4,186 J/kg·°C) × ([tex]T_f[/tex] - 0°C).
Similarly, we calculate the energy lost by the water as it cools down from 15.0°C to the final temperature:
Q₃ = (0.615 kg) × (4,186 J/kg·°C) × (15.0°C - [tex]T_f[/tex] ).
Since the total energy gained by the ice must be equal to the total energy lost by the water, we can equate the three equations:
[tex]Q_1 + Q_2 = Q_3[/tex]
Solving this equation, we find the final temperature [tex]T_f[/tex] to be 4.54°C.
To determine the amount of ice remaining at equilibrium, we consider the mass of ice that has melted and mixed with the water.
The total mass of the system at equilibrium will be the sum of the initial mass of water and the mass of melted ice:
615 g + (255 g - melted mass).
Since the melted ice has a density equal to that of water, the mass of melted ice is equal to its volume.
We can use the density formula:
density = mass/volume, to find the volume of melted ice.
Substituting the values, we have:
density of water = (255 g - melted mass) / volume of melted ice.
Solving for the volume of melted ice and substituting the density of water, we find the volume of melted ice to be
(255 g - melted mass) / 1 g/cm³.
Since the volume of melted ice is also equal to its mass, we can equate the volume of melted ice with the mass of melted ice:
(255 g - melted mass) / 1 g/cm³ = melted mass.
Solving this equation, we find the mass of melted ice to be 165.4 g.
Therefore, the amount of ice remaining at equilibrium is the initial mass of ice minus the mass of melted ice:
255 g - 165.4 g = 89.6 g.
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When the spin direction of the disk was changed, the direction of the precession also changed. Why?
When the add-on mass was placed on the opposite end of the gyroscope axle, the gyroscope rotated in reverse. Why?
Hint: direction of angular momentum of the disk, direction of torque
The change in the spin direction of the disk results in a change in the direction of precession due to the conservation of angular momentum.
Angular momentum is a vector quantity, meaning it has both magnitude and direction. It is given by the product of the moment of inertia and the angular velocity.
When the spin direction of the disk is changed, the angular momentum vector of the disk also changes direction. According to the conservation of angular momentum, the total angular momentum of the system must remain constant if no external torques act on it.
In the case of a gyroscope, the angular momentum is initially directed along the axis of rotation of the spinning disk.
When the spin direction of the disk is reversed, the angular momentum vector of the disk changes direction accordingly. To maintain the conservation of angular momentum, the gyroscope responds by changing the direction of its precession. This change occurs to ensure that the total angular momentum of the system remains constant.
Regarding the second scenario with the add-on mass placed on the opposite end of the gyroscope axle, the gyroscope rotates in reverse due to the torque applied to the system. Torque is the rotational equivalent of force and is responsible for changes in angular momentum. Torque is given by the product of the applied force and the lever arm distance.
By placing the add-on mass on the opposite end of the gyroscope axle, the torque acts in a direction opposite to the previous scenario. This torque causes the gyroscope to rotate in reverse, changing the direction of its precession. The direction of the torque determines the change in the gyroscope's rotational behavior.
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A plastic rod of length 1.88 meters contains a charge of 6.8nC. The rod is formed into semicircle What is the magnitude of the electric field at the center of the semicircle? Express your answer in NiC
A plastic rod of length 1.88 meters contains a charge of 6.8nC.The magnitude of the electric field at the center of the semicircle is approximately [tex]1.19 * 10^6 N/C[/tex]
To find the magnitude of the electric field at the center of the semicircle formed by a plastic rod, we can use the concept of electric field due to a charged rod.
The electric field at the center of the semicircle can be calculated by considering the contributions from all the charges along the rod. Since the rod is uniformly charged, we can divide it into infinitesimally small charge elements and integrate their contributions.
The formula for the electric field due to a charged rod at a point along the perpendicular bisector of the rod is:
E = (kλ / R) * (1 - cosθ)
Where E is the electric field, k is the electrostatic constant (9 x 10^9 Nm²/C²), λ is the linear charge density (charge per unit length), R is the distance from the rod to the point, and θ is the angle between the perpendicular bisector and a line connecting the point to the rod.
In this case, the rod is formed into a semicircle, so the angle θ is 90 degrees (or π/2 radians). The linear charge density λ can be calculated by dividing the total charge Q by the length of the rod L:
λ = Q / L
Plugging in the values:
λ = 6.8 nC / 1.88 m
Converting nC to C and m to meters:
λ = 6.8 x 10^(-9) C / 1.88 m
Now, we can calculate the electric field at the center of the semicircle by plugging in the values into the equation:
E = ([tex]9 * 10^9[/tex] Nm²/C²) * [tex]6.8 x 10^(-9)[/tex])C / 1.88 m) * (1 - cos(π/2))
Simplifying the equation:
E ≈ [tex]1.19 * 10^6 N/C[/tex]
Therefore, the magnitude of the electric field at the center of the semicircle is approximately [tex]1.19 * 10^6 N/C[/tex]
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The molar mass of argon is M = 40 x 10⁻³ kg/mol, and the molar mass of helium is M = 4 x 10⁻³ kg/mol. a) Find vᵣ ₘₛ for an argon atom if 1 mol of the gas is confined to a 1-liter container at a pressure of 10 atm. b) Find vᵣ ₘₛ for a helium atom under the same conditions and compare it to the value you calculated for argon. c) How much heat is removed when 100 g of steam at 150°C is cooled and frozen into 100 g of ice at 0°C. Note that the specific heat of ice is 2,010 J/kg·K and the specific heat of liquid water is 4,186 J/kg·K.
The root mean square velocity of an argon atom under the given conditions is approximately 226.23 m/s. The root mean square velocity for a helium atom under the given conditions is also approximately 226.23 m/s. The amount of heat removed when 100 g of steam at 150°C is cooled and frozen into 100 g of ice at 0°C is 661,300 J.
a) To find vᵣ ₘₛ for an argon atom if 1 mol of the gas is confined to a 1-liter container at a pressure of 10 atm, use the ideal gas law formula:
vᵣ ₘₛ = RT/P
where R is the gas constant, T is the temperature, and P is the pressure.
Given:
R = 8.31 J/(mol·K)
T = 273 K (room temperature)
P = 10 atm
vᵣ ₘₛ = (8.31 J/(mol·K) * 273 K) / (10 atm) ≈ 226.23 m/s
Therefore, the root mean square velocity of an argon atom under the given conditions is approximately 226.23 m/s.
b) For a helium atom under the same conditions, use the same formula:
vᵣ ₘₛ = RT/P
Substituting the values:
vᵣ ₘₛ = (8.31 J/(mol·K) * 273 K) / (10 atm) ≈ 226.23 m/s
The root mean square velocity for a helium atom under the given conditions is also approximately 226.23 m/s.
Comparing the values, it is seen that the root mean square velocities of argon and helium are the same.
c) To calculate the amount of heat removed when 100 g of steam at 150°C is cooled and frozen into 100 g of ice at 0°C, we need to consider two processes: cooling the steam and freezing the water.
Cooling the steam:
Q1 = m1 * c1 * ΔT1
where m1 is the mass, c1 is the specific heat capacity, and ΔT1 is the change in temperature.
Given:
m1 = 100 g
c1 (specific heat of steam) = 4,186 J/(kg·K)
ΔT1 = 150°C - 0°C = 150 K
Q1 = 100/1000 * 4,186 J/(kg·K) * 150 K = 627,900 J
Freezing the water:
Q2 = m2 * L
where m2 is the mass and L is the latent heat of fusion.
Given:
m2 = 100 g
L (latent heat of fusion) = 334,000 J/kg
Q2 = 100/1000 * 334,000 J/kg = 33,400 J
The total heat removed is the sum of Q1 and Q2:
Q = Q1 + Q2 = 627,900 J + 33,400 J = 661,300 J
Therefore, the amount of heat removed when 100 g of steam at 150°C is cooled and frozen into 100 g of ice at 0°C is 661,300 J.
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Answer the following question in a clear and neat manner, while maintaining the same numbering system. Show all calculations and conversions. 2.1 At 14 °C, 30.7g carbon dioxide gas creates pressure of 613 mm Hg, what is the volume of the gas? 2.2 A 5.00 L pocket of air at sea level has a pressure of 100 atm. Suppose the air pockets rise in the atmosphere to a certain height and expands to a volume of 13.00 L. What is the pressure of the air at the new volume?
2.3 What is the density of oxygen gas in a 1.5 L container with a pressure of 85 kPa at a temperature of 25 °C.
Volume of gas at 14 °C is 17.0 L.
The pressure of air at new volume is 38.46 atm
The density of oxygen gas in a 1.5 L container with a pressure of 85 kPa at a temperature of 25 °C is 1.11 g/L.
30.7 g carbon dioxide gas creates pressure of 613 mm Hg at 14 °C.
The ideal gas equation is given by PV = nRT Where,
P = Pressure in atmospheres
V = Volume in Liters
n = Number of moles
R = Ideal Gas Constant
T = Temperature in Kelvin
R = 0.0821 atm L mol^-1 K^-1
T = (14 + 273) K = 287 K
Pressure in mmHg is given, we need to convert it into atmospheres by dividing it by 760.613 mm Hg = (613 / 760) atm = 0.8065 atm
The molar mass of CO2 = 44 g/mol
Number of moles of CO2 = 30.7 g / 44 g/mol = 0.698 moles
Substituting the values in the ideal gas equation, we get
V = nRT / P= 0.698 mol x 0.0821 atm L mol^-1 K^-1 x 287 K / 0.8065 atm= 17.0 L
Volume of gas at 14 °C is 17.0 L
5.00 L pocket of air at sea level has a pressure of 100 atm. Suppose the air pockets rise in the atmosphere to a certain height and expands to a volume of 13.00 L.
Using Boyle’s Law,
P1V1 = P2V2 Where,
P1 = 100 atm
V1 = 5.00 L
P2 = ?
V2 = 13.00 L
P2 = P1V1 / V2 = 100 atm x 5.00 L / 13.00 L= 38.46 atm
The pressure of air at new volume is 38.46 atm.
Container volume, V = 1.5 L
Pressure, P = 85 kPa
Temperature, T = 25 °C = (25 + 273) K = 298 K
The ideal gas equation is given by PV = nRT Where,
P = Pressure in atmospheres
V = Volume in Liters
n = Number of moles
R = Ideal Gas Constant
T = Temperature in Kelvin
R = 0.0821 atm L mol^-1 K^-1
The molar mass of O2 = 32 g/mol
Number of moles of O2 = PV / RT= (85 x 10^3 Pa x 1.5 x 10^-3 m^3) / (8.31 J K^-1 mol^-1 x 298 K)= 0.0518 moles
Density, d = mass / volume
The mass of O2 = 0.0518 moles x 32 g/mol = 1.66 g
Density, d = 1.66 g / 1.5 L= 1.11 g/L
The density of oxygen gas in a 1.5 L container with a pressure of 85 kPa at a temperature of 25 °C is 1.11 g/L.
Thus,
Volume of gas at 14 °C is 17.0 L.
The pressure of air at new volume is 38.46 atm
The density of oxygen gas in a 1.5 L container with a pressure of 85 kPa at a temperature of 25 °C is 1.11 g/L.
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Imagine you're an astronaut working on the new space station in orbit around Mars While working a distance 154 m from the station, your cool little jet pack goes out and you have no way to get back to safely. Fortunately, you're a physics fan so you calmly and cooly use that knowledge and loss your 18 kg jetpack at a speed of 19 m/s directly away from the station to make your way back to safety Part A How long does it take you to reach the space station after the jetpack leaves your hands? Assume that the combined mass of you and your space suite is 100 kg NoteBe sure to round to the appropriate number of significant figures as the final step of your calculation before submitting your response unde vado reset keyboard shortcuts help Value Units
After losing your 18 kg jetpack at a speed of 19 m/s away from the space station, it will take approximately 45.0 seconds for you to reach the station.
To calculate the time it takes for you to reach the space station, we can apply the principle of conservation of momentum. Initially, the total momentum of the system (you and your jetpack) is zero since you are at rest relative to the space station.
When you release the jetpack, it gains momentum in one direction, causing you to gain an equal amount of momentum in the opposite direction.
The conservation of momentum equation can be written as:
m1 * v1 = m2 * v2
where m1 and v1 are the mass and velocity of the jetpack, and m2 and v2 are the mass and velocity of you and your space suit.
Substituting the given values (m1 = 18 kg, v1 = -19 m/s, m2 = 100 kg), we can solve for v2, the velocity of you and your space suit after releasing the jetpack. Rearranging the equation, we have:
v2 = (m1 * v1) / m2
v2 = (18 kg * -19 m/s) / 100 kg
v2 = -3.42 m/s
Since you and your space suit are initially at rest, the final velocity is equal to the relative velocity between you and the space station. The distance between you and the station is 154 m, and to find the time it takes to cover this distance, we use the equation:
time = distance / velocity
time = 154 m / 3.42 m/s
time ≈ 45.0 seconds
Rounding to the appropriate number of significant figures, it will take approximately 45.0 seconds for you to reach the space station after the jetpack leaves your hands.
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Charles Cansado launched a 100 g dart upwards from a height of 150 cm using a toy gun. The stiffness of the gun's spring is 1 000 N/m which was compressed 10 cm. Determine the impact velocity of the dart the instant it reaches its target at a height of 450 cm if the heat loss was 0.588 J. Determine the percentage efficiency of the shot.
The impact velocity of the dart when it reaches its target at a height of 450 cm is 5.20 m/s. The percentage efficiency of the shot is 95.2%.
In order to determine the impact velocity of the dart, we can use the principle of conservation of mechanical energy. The initial potential energy of the dart is given by mgh, where m is the mass of the dart (0.1 kg), g is the acceleration due to gravity (9.8 m/s^2), and h is the initial height (1.5 m). The final potential energy of the dart is mgh, where h is the final height (4.5 m). The initial kinetic energy of the dart is zero, as it was launched from rest. Therefore, the final kinetic energy of the dart is equal to the difference between the initial potential energy and the heat loss (0.588 J). Using these values, we can calculate the final velocity of the dart using the equation KE = 0.5mv^2, where KE is the kinetic energy, m is the mass of the dart, and v is the velocity.
The percentage efficiency of the shot can be determined by calculating the ratio of the actual energy output (final kinetic energy) to the theoretical maximum energy output (initial potential energy). The efficiency is then multiplied by 100 to express it as a percentage. In this case, the efficiency is 95.2%. This means that 95.2% of the energy stored in the spring was transferred to the dart as kinetic energy, while the remaining 4.8% was lost as heat.
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