To develop this problem it is necessary to apply the concepts related to the Aerodynamic Drag Force.
By definition the Drag Force is defined as
[tex]F_D = \frac{1}{2} \rho A C_D v^2[/tex]
Where,
A = Area
[tex]\rho[/tex]= Density
[tex]C_d[/tex] = Drag coefficient
v = Velocity
According to our values we have,
[tex]A = 1.8*1.8=3.24m^2[/tex]
[tex]C_D = 1.4[/tex]
[tex]V = 5m/s[/tex]
Replacing we have
[tex]F_D = \frac{1}{2} 1.23*3.24*1.4*5^2[/tex]
[tex]F_D = 69.74[/tex]
By definition we know that the thermal energy is given by the force applied in a given displacement then
[tex]W = F*d[/tex]
[tex]W = 69.74*200[/tex]
[tex]W = 13948J[/tex]
Therefore the thermal energy is added to the air by the drag force is 13.9kJ
The thermal energy added to the air by the drag force from a runner's parachute can be calculated by determining the work done against this force during a run. This involves first calculating the drag force with known parameters, then using the force to calculate the work done over the run's distance. This quantity represents the thermal energy imparted to the air.
Explanation:The calculation for thermal energy added to the air by the drag force requires understanding the basic principles of work and energy. The work done by the drag force is given by the formula W = Fd, where W is work, F is force, and d is distance. In this case, the force is the drag force internalized by the parachute. The drag force is calculated using the equation F = 0.5 * p * v² * C * A, where:
By substituting these values into the formula, we can compute the drag force. Thereafter, we can use this force in our initial work equation to calculate the work done over a 200 m run. It's important to note that the work done against the drag force is transformed into heat (thermal energy). Thus, the work done equals the thermal energy added to the air by the drag force.
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Burns produced by steam at 100°C are much more severe than those produced by the same mass of 100°C water. Calculate the quantity of heat in (Cal or kcal) that must be removed from 6.1 g of 100°C steam to condense it and lower its temperature to 46°C. Specific heat of water = 1.00 kcal/(kg · °C); heat of vaporization = 539 kcal/kg; specific heat of human flesh = 0.83 kcal/(kg · °C).
To calculate the quantity of heat that must be removed from 6.1 g of 100°C steam, we need to consider both the change in temperature and the phase change from steam to liquid. The specific heat of water is used to calculate the heat required to lower the temperature, while the heat of vaporization is used to calculate the heat required to condense the steam. Adding these two heat values together gives us the total amount of heat that must be removed from the steam, which is approximately 3.61164 kcal.
Explanation:When steam at 100°C condenses and its temperature is lowered to 46°C, heat must be removed from the steam. To calculate the amount of heat, we can use the specific heat of steam and the latent heat of vaporization. First, we calculate the heat required to lower the temperature of the steam from 100°C to 46°C using the specific heat of water. We then calculate the heat required to condense the steam using the latent heat of vaporization. Finally, we add these two heat values together to obtain the total amount of heat that must be removed from the steam.
Given:
Mass of steam = 6.1 gTemperature change = 100°C - 46°C = 54°CSpecific heat of water = 1.00 kcal/(kg · °C)Heat of vaporization = 539 kcal/kg
Calculations:
Calculation:
Q1 = 0.32874 kcalQ2 = 3.2829 kcalQ = Q1 + Q2 = 0.32874 kcal + 3.2829 kcal = 3.61164 kcal
Therefore, the quantity of heat that must be removed from 6.1 g of 100°C steam to condense it and lower its temperature to 46°C is approximately 3.61164 kcal.
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To condense and cool 6.1 g of 100°C steam to 46°C, 3.2879 kcal must be removed for condensation, and 0.3304 kcal for cooling, for a total of 3.6183 kcal.
Explanation:Calculating the Quantity of Heat for Condensation and Cooling
To calculate the quantity of heat that must be removed from 6.1 g of 100°C steam to condense it and lower its temperature to 46°C, we need to consider two processes: condensation and cooling. For condensation, we use the heat of vaporization, and for cooling, we use the specific heat of water.
Calculate the heat released during condensation of steam into water at 100°C:Total heat removed is the sum of the heat from both steps: 3.2879 kcal + 0.3304 kcal = 3.6183 kcal.
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If the surface temperature of that person's skin is 30∘C (that's a little lower than healthy internal body temperature because your skin is usually a little colder than your insides), what is the total power that person will radiate? For now, assume the person is a perfect blackbody (so ϵ=1).
Answer:
[tex]E=477.92\ W.m^{-2}[/tex]
Explanation:
Given that:
Absolute temperature of the body, [tex]T=273+30=303\ K[/tex]
emissivity of the body, [tex]\epsilon=1[/tex]Using Stefan Boltzmann Law of thermal radiation:
[tex]E=\epsilon. \sigma.T^4[/tex]
where:
[tex]\sigma =5.67\times 10^{-8}\ W.m^{-2}.K^{-4}[/tex] (Stefan Boltzmann constant)
Now putting the respective values:
[tex]E=1\times 5.67\times 10^{-8}\times 303^4[/tex]
[tex]E=477.92\ W.m^{-2}[/tex]
g A four bladed propeller on a cargo aircraft has a moment of inertia of 40 kg m2. If the prop goes from rest to 400 rpm in 14 sec, findA) the torque required andB) the number of revolutions turned as the prop achieves operating speed.
Answer:
a. T = 119.68 N.m
b. r = 140 rev
Explanation:
first we know that:
∑T = Iα
where ∑T is the sumatory of the torques, I is the moment of inertia and α is the angular aceleration.
so, if the prop goes from rest to 400 rpm in 14 seconds we can find the α of the system:
1. change the 400 rpm to radians as:
W = 400*2π/60
W = 41.888 rad /s
2. Then, using the next equation, we find the α as:
w = αt
solving for α
α = [tex]\frac{w}{t}[/tex]
note: t is the time, so:
α = [tex]\frac{41.888}{14}[/tex]
α = 2.992 rad/s^2
Now using the first equation, we get:
T = Iα
T = 40(2.992)
T = 119.68 N.m
On the other hand, for know the the number of revolutions turned as the prop achieves operating speed, we use the following equation:
θ = wt +[tex]\frac{1}{2}[/tex]α[tex]t^2[/tex]
Where w = 41.888 rad /s, α = 2.992 rad/s^2, t is the time and θ give as the number of radians that the prop made in the fisrt 14 seconds, so:
θ = (41.888)(14)+[tex]\frac{1}{2}[/tex](2.992)(14[tex])^2[/tex]
θ = 879.648 rad
and that divided by 2π give us the number of revolutions r, so:
r = 140 rev
During the 2007 French Open, Venus Williams hit the fastest recorded serve in a premier women’s match, reaching a speed of 58 m/s (209 km/h).
What is the average force exerted on the 0.057-kg tennis ball by Venus Williams’ racquet, assuming that the ball’s speed just after impact is 58 m/s, that the initial horizontal component of the velocity before impact is negligible, and that the ball remained in contact with the racquet for 5.0 ms (milliseconds)?
a)660 N
b)1660 N
c)25 N
d)4000 N
Final answer:
The average force exerted on the tennis ball by Venus Williams' racquet during her serve is calculated using the formula F = Δp/Δt, resulting in approximately 660 N, with the correct answer being option a).
Explanation:
The question relates to determining the average force exerted by Venus Williams' racquet on a tennis ball during her serve at the 2007 French Open. To find the average force, we can use the formula derived from Newton's second law of motion, F = ma. However, instead of finding the acceleration first, we use the formula F = Δp/Δt (force is the change in momentum over the change in time), because we know the velocity after impact and the time of contact.
The initial momentum (pi) is 0, as the initial velocity is negligible, so the final momentum (pf) is mv, where m is the mass of the tennis ball (0.057 kg) and v is the final velocity (58 m/s). As the time of contact with the racquet is 5.0 ms (or 0.005 seconds), we calculate the force as follows:
F = (m × v)/Δt = (0.057 kg × 58 m/s)/0.005 s = (3.306 kg·m/s)/0.005 s = 661.2 N
Therefore, the correct answer is approximately 660 N, which matches option a).
As a new electrical technician, you are designing a large solenoid to produce a uniform 0.150-T magnetic field near the center of the solenoid. You have enough wire for 3100 circular turns. This solenoid must be 57.0 cm long and 7.00 cm in diameter.What current will you need to produce the necessary field?
Answer:
I = 21.94 A
Explanation:
Given that
B= 0.15 T
Number of turns N= 3100
Length L = 57 cm
Diameter ,d= 7 cm
We know that magnetic field in the solenoid given as
[tex]B=\dfrac{\mu_0IN}{L}[/tex]
[tex]I=\dfrac{BL}{\mu_0N}[/tex]
Now by putting the values
[tex]I=\dfrac{0.15\times 0.57}{4\pi \times 10^{-7}\times 3100}[/tex]
I = 21.94 A
Therefore current need to produce 0.15 T magnetic filed is 21.94 A.
Fish are hung on a spring scale to determine their mass. (a) What is the force constant of the spring in such a scale if the spring stretches 8.00 cm for a 10.0 kg load? (b) What is the mass of a fish that stretches the spring 5.50 cm? (c) How far apart are the half-kilogram marks on the scale?
a) The spring constant is 1225 N/m
b) The mass of the fish is 6.88 kg
c) The marks are 0.4 cm apart
Explanation:
a)
When the spring is at equilibrium, the weight of the load applied to the spring is equal (in magnitude) to the restoring force of the spring, so we can write
[tex]mg = kx[/tex]
where
m is the mass of the load
[tex]g=9.8 m/s^2[/tex] is the acceleration of gravity
k is the spring constant
x is the stretching of the spring
For the load in this problem we have
m = 10.0 kg
x = 8.00 cm = 0.08 m
Substituting, we find the spring constant
[tex]k=\frac{mg}{x}=\frac{(10)(9.8)}{0.08}=1225 N/m[/tex]
b)
As before, at equilibrium, the weight of the fish must balance the restoring force in the spring, so we have
[tex]mg=kx[/tex]
where this time we have:
m = mass of the fish
[tex]g=9.8 m/s^2[/tex]
k = 1225 N/m is the spring constant
x = 5.50 cm = 0.055 m is the stretching of the spring
Substituting,
[tex]m=\frac{kx}{g}=\frac{(1225)(0.055)}{9.8}=6.88 kg[/tex]
c)
To solve this part, we just need to find the change in stretching of the spring when a load of half-kilogram is hanging on the spring. Using again the same equation,
[tex]mg=kx[/tex]
where this time we have:
m = 0.5 kg
[tex]g=9.8 m/s^2[/tex]
k = 1225 N/m
x = ? is the distance between the half-kilogram marks on the scale
Substituting,
[tex]x=\frac{mg}{k}=\frac{(0.5)(9.8)}{1225}=0.004 m = 0.4 cm[/tex]
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An astronaut goes out for a space walk. Her mass (including space suit, oxygen tank, etc.) is 100 kg. Suddenly, disaster strikes and her tether line becomes disconnected, so she is stuck at rest a distance x away from the space craft!
Luckily, you have to know physics to be an astronaut. The astronaut takes off her 15 kg oxygen tank and throws it away from the spacecraft with a speed of 10 m/s. Due to conservation of momentum, she is propelled towards the spacecraft.
The astronaut has 1.5 minutes of oxygen remaining in her space suit to get her back to the craft. What is the maximum distance the astronaut can be away from the spacecraft to make it back before she runs out of oxygen?
Part A: What are the Known Variables and Unknown Variables? list them.
Part B: What are the equations needed to solve this problem?
Part C: Solve the problem.
Answer:
Part A:
Unknown variables:
velocity of the astronaut after throwing the tank.
maximum distance the astronaut can be away from the spacecraft to make it back before she runs out of oxygen.
Known variables:
velocity and mass of the tank.
mass of the astronaut after and before throwing the tank.
maximum time it can take the astronaut to return to the spacecraft.
Part B:
To obtain the velocity of the astronaut we use this equation:
-(momentum of the oxygen tank) = momentum of the astronaut
-mt · vt = ma · vt
Where:
mt = mass of the tank
vt = velocity of the tank
ma = mass of the astronaut
va = velocity of the astronaut
To obtain the maximum distance the astronaut can be away from the spacecraft we use this equation:
x = x0 + v · t
Where:
x = position of the astronaut at time t.
x0 = initial position.
v = velocity.
t = time.
Part C:
The maximum distance the astronaut can be away from the spacecraft is 162 m.
Explanation:
Hi there!
Due to conservation of momentum, the momentum of the oxygen tank when it is thrown away must be equal to the momentum of the astronaut but in opposite direction. In other words, the momentum of the system astronaut-oxygen tank is the same before and after throwing the tank.
The momentum of the system before throwing the tank is zero because the astronaut is at rest:
Initial momentum = m · v
Where m is the mass of the astronaut plus the equipment (100 kg) and v is its velocity (0 m/s).
Then:
initial momentum = 0
After throwing the tank, the momentum of the system is the sum of the momentums of the astronaut plus the momentum of the tank.
final momentum = mt · vt + ma · va
Where:
mt = mass of the tank
vt = velocity of the tank
ma = mass of the astronaut
va = velocity of the astronaut
Since the initial momentum is equal to final momentum:
initial momentum = final momentum
0 = mt · vt + ma · va
- mt · vt = ma · va
Now, we have proved that the momentum of the tank must be equal to the momentum of the astronaut but in opposite direction.
Solving that equation for the velocity of the astronaut (va):
- (mt · vt)/ma = va
mt = 15 kg
vt = 10 m/s
ma = 100 kg - 15 kg = 85 kg
-(15 kg · 10 m/s)/ 85 kg = -1.8 m/s
The velocity of the astronaut is 1.8 m/s in direction to the spacecraft.
Let´s place the origin of the frame of reference at the spacecraft. The equation of position for an object moving in a straight line at constant velocity is the following:
x = x0 + v · t
where:
x = position of the object at time t.
x0 = initial position.
v = velocity.
t = time.
Initially, the astronaut is at a distance x away from the spacecraft so that
the initial position of the astronaut, x0, is equal to x.
Since the origin of the frame of reference is located at the spacecraft, the position of the spacecraft will be 0 m.
The velocity of the astronaut is directed towards the spacecraft (the origin of the frame of reference), then, v = -1.8 m/s
The maximum time it can take the astronaut to reach the position of the spacecraft is 1.5 min = 90 s.
Then:
x = x0 + v · t
0 m = x - 1.8 m/s · 90 s
Solving for x:
1.8 m/s · 90 s = x
x = 162 m
The maximum distance the astronaut can be away from the spacecraft is 162 m.
Medical cyclotrons need efficient sources of protons to inject into their center. In one kind of ion source, hydrogen atoms (i.e., protons with one orbiting electron) are fed into a chamber where there is a strong magnetic field. Electrons in this chamber are trapped in tight orbits, which greatly increases the chance that they will collide with a hydrogen atom and ionizes it. One such source uses a magnetic field of 90 mT, and the electrons' kinetic energy is 2.0 eV.If the electrons travel in a plane perpendicular to the field, what is the radius of their orbits?
Answer:
Explanation:
Electron's kinetic energy = 2 eV
= 2 x 1.6 x 10⁻¹⁹ J
1/2 m v² = 3.2 x 10⁻¹⁹
1/2 x 9.1 x 10⁻³¹ x v² = 3.2 x 10⁻¹⁹
v² = .703 x 10¹²
v = .8385 x 10⁶ m/s
Electrons revolve in a circular orbit when forced to travel in a magnetic field whose radius can be expressed as follows
r = mv / Bq
where m , v and q are mass , velocity and charge of electron .
here given magnetic field B = 90 mT
= 90 x 10⁻³ T
Putting these values in the expression above
r = mv / Bq
= [tex]\frac{9\times10^{-31}\times.8385\times10^6}{90\times10^{-3}\times1.6\times10^{-19}}[/tex]
= .052 mm.
If there were a great migration of people toward the Earth's equator, the length of the day would
a. decrease because of conservation of angular momentum.
b. remain unaffected.
c. increase because of conservation of angular momentum.
d. decrease because of conservation of energy.
e. increase because of conservation of energy.
Answer:
C. increase because of conservation of angular momentum.
Explanation:
We know that if there is no any external torque on the system then the angular momentum of the system will be conserved.
Angular momentum L
L = I ω
I=Mass moment of inertia , ω=Angular speed
If angular momentum is conserved
I₁ω₁ = I₂ω₂
If people migrates towards Earth's equator then mass moment of inertia will increases.
I₂ > I₁
Then we can say that ω₁ > ω₂ ( angular momentum is conserve)
We know that time period T given as
[tex]T=\dfrac{2\pi}{\omega}[/tex]
[tex]T_1=\dfrac{2\pi}{\omega_1}[/tex]
[tex]T_2=\dfrac{2\pi}{\omega_2}[/tex]
If ω₂ decrease then T₂ will increase .It means that length of the day will increase.
Therefore answer is C.
If a large number of people migrated towards the Earth's equator, the day length would remain largely unaffected. This is due to the law of conservation of angular momentum, considering the insignificant change to the Earth's total mass.
Explanation:The scenario mentioned in the question refers to a law in physics called the conservation of angular momentum. The length of a day on Earth is predominantly determined by how fast our planet spins on its axis. If there were a large migration of people towards the Earth's equator, hypothetically, the day length would remain largely unaffected. The mass of the people in this context is insignificant when compared to the total mass of the Earth. As such, their migration would not have a noticeable impact on Earth's rotational speed due to conservation of angular momentum. Therefore, the correct answer is that the length of the day would remain unaffected (option b).
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A guitar string is plucked and set into vibration. The vibrating string disturbs the surrounding air, resulting in a sound wave. Which of the following is correct? Group of answer choices If the temperature of air changes, the speed of the Wave in the string Doesn't change, but the speed of the Sound wave in air changes . Both the Wave in the string and the Sound wave in air are transverse waves . Both the Wave in the string and the Sound wave in air are longitudinal waves . The Wave in the string is longitudinal , the Sound wave in air is transverse .
Answer:
a) True. The speed of the wave in the string does not depend on the temperature, but the speed of the wave the air depends on the Temperatue.
Explanation:
Let's analyze the vibration of the string, when the string is touched a transverse wave is produced whose speed is determined by the tension and density of the string
V = √T/μ
This wave advances and bounces at one of the ends forming a standing wave that induces a vibration in the surrounding air that therefore also produces a longitudinal wave whose velocity is a function of time
v = 331 √( 1+ T/273)
With this information we can review the statements given
a) True. The speed of the wave in the string does not depend on the temperature, but the speed of the wave the air depends on the Temperatue.
b) False. The wave in the string is transverse, but the wave in the air is longitudinal
c) False. The wave in the string is transverse
d) False. It's the other way around
Answer:
A
Explanation:
Just got it right on edge
The earth is about 1.50 X 1011 m from the sun and has a period of about 365 days orbiting around the sun. Suppose that the orbit of the earth is circular, what is the magnitude of the acceleration of the earth in m/s2?
To solve this problem it is necessary to apply the concepts presented in Kepler's third law in which the period is described, as well as the theorems developed for acceleration based on gravity.
Acceleration in gravitational terms can be expressed as
[tex]a = \frac{GM}{r^2}[/tex]
Where,
G = Gravitational Universal Constant
M = Mass of Earth
r = Distance
At the same time the Period by Kepler's law the Period is described as
[tex]T^2 = \frac{4\pi^2r^3}{GM}[/tex]
That is equal to
[tex]T^2 = \frac{4\pi^2r}{\frac{GM}{r^2}}[/tex]
Using the equation of acceleration,
[tex]T^2 = \frac{4\pi^2r}{a}[/tex]
Re-arrange to find a,
[tex]a = \frac{4\pi^2r}{T^2}[/tex]
Our values are given as
[tex]r = 1.5*10^{11}m[/tex]
[tex]T = 365days(\frac{86400s}{1days}) = 31536000s[/tex]
Replacing we have,
[tex]a = \frac{4\pi^2r}{T^2}[/tex]
[tex]a = \frac{4\pi^2(1.5*10^{11})}{(31536000)^2}[/tex]
[tex]a = 0.005954m/s^2[/tex]
Therefore the magnitude of the acceleration of the earth is [tex]0.005954m/s^2[/tex]
The magnitude of the acceleration of the Earth in its orbit around the sun, assuming a circular orbit, is approximately 0.0059 m/s².
Explanation:The concept at play here is centripetal acceleration, which is the rate of change of tangential velocity and points toward the center of the circle around which Earth, or any object, orbits. For Earth orbiting the sun, we can use the formula ac = v²/r (where v is velocity, r is radius), but given that v isn't directly stated, one must compute it first by v = 2πr/T (where T is the period of the orbit in seconds).
So, the velocity of the Earth in its orbit is approximated as 2π(1.50x10¹¹ m)/(365.25x24x60x60 s) = 29,785.6 m/s. To get the acceleration, plug this computed v value into the ac equation: ac = (29,785.6 m/s)²/(1.50 x 10¹¹ m) = 0.0059 m/s².
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2. A package with a heat sink and fan has a thermal resistance to the ambient of 8 °C/W. The thermal resistance from the die to the package is 2 °C/W. If the package is in a chassis that will never exceed 50 °C and the maximum acceptable die temperature is 110 °C, how much power can the chip dissipate?
To solve this problem it is necessary to apply the concepts related to the Power depending on the temperature and the heat transferred.
By definition the power can be expressed as
[tex]P = \frac{\Delta T}{\Delta Q}[/tex]
Where,
[tex]\Delta T = T_m - T_a =[/tex] Change at the temperature, i.e, the maximum acceptable die temperature ([tex]T_m[/tex]) with the allowable temperature in chassis ([tex]T_A[/tex])
[tex]\Delta Q = Q_A-Q_D =[/tex] Change in the thermal resistance to ambient ([tex]Q_A[/tex]) and the Thermal resistance from die to package ([tex]Q_D[/tex])
Our values are given as,
[tex]T_m=110\°C[/tex]
[tex]T_a= 50\°C[/tex]
[tex]Q_A= 8\°C/W[/tex]
[tex]Q_D= 2\°C/W[/tex]
Replacing we have,
[tex]P = \frac{110-50}{8-2}[/tex]
[tex]P = 10W[/tex]
The power that can dissipate the chip is 10W
Calculate the minimum average power output necessary for a person to run up a 12.0 m long hillside, which is inclined at 25.0° above the horizontal, in 3.00 s. You can neglect the person's kinetic energy. Express your answer in horsepower
Answer:
Power, P = 924.15 watts
Explanation:
Given that,
Length of the ramp, l = 12 m
Mass of the person, m = 55.8 kg
Angle between the inclined plane and the horizontal, [tex]\theta=25^{\circ}[/tex]
Time, t = 3 s
Let h is the height of the hill from the horizontal,
[tex]h=l\ sin\theta[/tex]
[tex]h=12\times \ sin(25)[/tex]
h = 5.07 m
Let P is the power output necessary for a person to run up long hill side as :
[tex]P=\dfrac{E}{t}[/tex]
[tex]P=\dfrac{mgh}{t}[/tex]
[tex]P=\dfrac{55.8\times 9.8\times 5.07}{3}[/tex]
P = 924.15 watts
So, the minimum average power output necessary for a person to run up is 924.15 watts. Hence, this is the required solution.
We find the height of the 25° incline and then calculate the potential energy per kg, which is then turned into power by dividing by time. The result is 16.6 W or 0.022 hp. Therefore, the minimum average power output necessary for a person to run up a 12.0 m, 25° long hillside in 3.00 s is approximately 2.2% of a horsepower.
Explanation:This problem is solved in several steps. First, we need to determine the potential energy gain of the person running up the hillside. The formula for potential energy (PE) is PE = m*g*h, where m is mass, g is gravity (approximately 9.8 m/s²), and h is the height of the hill. Since we're not given the person's mass, we'll imagine the person has a mass of 1 kg just to calculate the potential energy gain per kg, but it isn't necessary to know the exact weight for calculating the minimum average power.
The height of the incline is given by 12.0m*sin(25°) = 5.09 m. So, the potential energy gain is PE = 1 kg * 9.8 m/s² * 5.09 m = 49.88 J. Converting this to power (P) by dividing energy by time, P = 49.88 J / 3.0 s = 16.6 W.
Since one horsepower (hp) is approximately 746 watts (W), the power in horsepower is 16.6 W / 746 W/hp = 0.022 hp, or 2.2% of a horsepower. This is the minimum average power output required for a person to climb this hill in 3 seconds.
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A circular copper disk of diameter D=10 cm rotates at frequency =1800 rev/min about an axis through its center and at right angles to the disk. A uniform magnetic field B of 10,000 gauss is perpendicular to the disk. What potential difference e develops between the axis of the disk and its rim?
Answer:
e=2356.125 V
Explanation:
Given that
D= 10 cm = 0.1 m
R= 0.05
B= 10,000
Angular speed ,ω = 1800 rev/min
Speed in rad/s given as
[tex]\omega =\dfrac{2\pi N}{60}[/tex]
[tex]\omega =\dfrac{2\pi \times 1800}{60}[/tex]
ω= 188.49 rad/s
The potential difference given as
e= B R v
v=average speed
[tex]v=\dfrac{\omega}{2}R[/tex]
[tex]e=\dfrac{B}{2}R^2 {\omega}[/tex]
By putting the values
[tex]e=\dfrac{10000}{2}0.05^2 \times {188.49}[/tex]
e=2356.125 V
A proton moves through a uniform magnetic field given by vector B = (10 i hat- 24.0 j hat + 30 k hat) mT. At time t1, the proton has a velocity given by vector v = v x i hat + vy j hat + (2000 m/s) k hat and the magnetic force on the proton is vector Fb = (3.82x10-17 N) i hat + (1.59x10-17 N) j hat. (a) At that instant, what is vx? m/s (b) What is vy?
a. The value of vₓ = 33.77 km/s
b. The value of Vy = 81.05 km/s
The magnetic force on the proton
The magnetic force, F on the proton moving in the uniform magnetic field is given by
F = qv × B where
F = force on proton = (3.82 × 10⁻¹⁷ N)l + (1.59 × 10⁻¹⁷ N)j + 0k, q = charge on proton = 1.602 × 10⁻¹⁹ C, v = velocity of proton = Vxl + Vyj + (2000 m/s)k and B = magnetic field = (10i - 24.0j + 30k) mT = (10i - 24.0j + 30k) × 10⁻³ TRe-writing the force in matrix form, we have
[tex]\left[\begin{array}{ccc}F_{x} &F_{y} &F_{z} \\\end{array}\right] = q\left[\begin{array}{ccc}i&j&k\\v_{x} &v_{y}&v_{z}\\B_{x}&B_{y}&B_{z}\end{array}\right][/tex]
Taking the determinant, we have
[tex]F_{x}i + F_{y}j + F_{z}k = q[(v_{y}B_{z} - v_{z}B_{y})]i + q[(v_{x}B_{z} - v_{z}B_{x})]j + q[(v_{x}B_{y} - v_{y}B_{x})]k[/tex]
Equating the components of the force, we have
[tex]F_{x} = q[(v_{y}B_{z} - v_{z}B_{y})] (1)\\F_{y} = q[(v_{x}B_{z} - v_{z}B_{x})] (2)\\F_{z} = q[(v_{x}B_{y} - v_{y}B_{x})] (3)[/tex]
[tex]F_{x}/q = [(v_{y}B_{z} - v_{z}B_{y})] (4)\\F_{y}/q = [(v_{x}B_{z} - v_{z}B_{x})] (5)\\F_{z}/q = [(v_{x}B_{y} - v_{y}B_{x})] (6)[/tex]
Since F = (3.82 × 10⁻¹⁷ N)l + (1.59 × 10⁻¹⁷ N)j + 0k, equation (5) and (6) become
[tex]1.59 X 10^{-17} /1.602 X 10^{-19} = [(v_{x}B_{z} - v_{z}B_{x})] (5)\\993 = [(v_{x}B_{z} - v_{z}B_{x})] (7)\\Also\\0/q = [(v_{x}B_{y} - v_{y}B_{x})] (6)\\0 = (v_{x}B_{y} - v_{y}B_{x}) \\v_{x}B_{y} = v_{y}B_{x}\\v_{y} = \frac{v_{x}B_{y}}{B_{x}} (8)[/tex]
a. The value of VxThe value of vₓ = 33.77 km/s
Since [tex]B_{x}[/tex] = 10 × 10 ⁻³ T, [tex]B_{z}[/tex] = 30 × 10 ⁻³ T and [tex]v_{z}[/tex] = 2000 m/s, substituting the values of the variables into equation (7), we have
[tex]v_{x}B_{z} - v_{z}B_{x} = 993 (7)[/tex]
vₓ(30 × 10 ⁻³ T) - 2000 m/s × 10 × 10 ⁻³ T = 993 N
vₓ(30 × 10 ⁻³ T) - 20 m/sT = 993 N
vₓ(30 × 10 ⁻³ T) = 993 N + 20 m/sT
vₓ(30 × 10 ⁻³ T) = 1013 N
vₓ = 1013 N/(30 × 10 ⁻³ T)
vₓ = 33.77 × 10³ m/s
vₓ = 33.77 km/s
So, the value of vₓ = 33.77 km/s
b. The value of VyThe value of Vy = 81.05 km/s
Since [tex]B_{x}[/tex] = 10 × 10 ⁻³ T, [tex]B_{y}[/tex] = 24.0 × 10 ⁻³ T and [tex]v_{x}[/tex] = 33.77 × 10³ m/s, substituting the values of the variables into equation (8), we have
[tex]v_{y} = \frac{v_{x}B_{y}}{B_{x}} (8)[/tex]
Vy = 33.77 × 10³ m/s × 24.0 × 10 ⁻³ T/10 × 10 ⁻³ T
Vy = 810.48 m/sT/10 × 10 ⁻³ T
Vy = 81.048 × 10³ m/s
Vy ≅ 81.05 km/s
So, the value of Vy = 81.05 km/s
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A lightning flash releases about 1010J of electrical energy. Part A If all this energy is added to 50 kg of water (the amount of water in a 165-lb person) at 37∘C, what are the final state and temperature of the water? The specific heat of water is 4180 J/kg⋅ ∘C, heat of vaporization at the boiling temperature for water is 2.256×106J/kg, the specific heat of steam is 1970 J/kg⋅ ∘C.
Answer:
water is in the vapor state,
Explanation:
We must use calorimetry equations to find the final water temperatures. We assume that all energy is transformed into heat
E = Q₁ + [tex]Q_{L}[/tex]
Where Q1 is the heat required to bring water from the current temperature to the boiling point
Q₁ = m [tex]c_{e}[/tex] ( [tex]T_{f}[/tex] -T₀)
Q₁ = 50 4180 (100 - 37)
Q₁ = 1.317 10⁷ J
Let's calculate the energy so that all the water changes state
[tex]Q_{L}[/tex] = m L
[tex]Q_{L}[/tex] = 50 2,256 106
[tex]Q_{L}[/tex] = 1,128 10⁸ J
Let's look for the energy needed to convert all the water into steam is
Qt = Q₁ + [tex]Q_{L}[/tex]
Qt = 1.317 107 + 11.28 107
Qt = 12,597 10⁷ J
Let's calculate how much energy is left to heat the water vapor
ΔE = E - Qt
ΔE = 10¹⁰ - 12,597 10⁷
ΔE = 1000 107 - 12,597 107
ΔE = 987.4 10⁷ J
With this energy we heat the steam, clear the final temperature
Q = ΔE = m [tex]c_{e}[/tex] ( [tex]T_{f}[/tex]-To)
( [tex]T_{f}[/tex]-T₀) = ΔE / m [tex]c_{e}[/tex]
[tex]T_{f}[/tex] = T₀ + ΔE / m [tex]c_{e}[/tex]
[tex]T_{f}[/tex] = 100 + 987.4 10⁷ / (50 1970)
[tex]T_{f}[/tex] = 100 + 1,002 10⁵
[tex]T_{f}[/tex] = 1,003 10⁵ ° C
This result indicates that the water is in the vapor state, in realizing at this temperature the water will be dissociated into its hydrogen and oxygen components
Calculating the final state and temperature of 50 kg of water at 37°C with 10¹°J of energy involves determining the energy needed to heat the water to 100°C and the energy to vaporize it. Using the given specific heat of water, heat of vaporization, and specific heat of steam, one can find whether all the water turns to steam and whether any energy is left to further heat the steam.
Explanation:If a lightning flash releases about 1010J of electrical energy, and all this energy is added to 50 kg of water at 37°C, we can determine the final state and temperature of the water. Given that the specific heat of water is 4180 J/kg·°C, the heat of vaporization at the boiling temperature for water is 2.256×106J/kg, and the specific heat of steam is 1970 J/kg·°C, these values can be used to calculate the amount of water that can be heated, brought to a boil, and then completely turned to steam. We can break this problem down into different stages, each requiring a certain amount of energy.
Firstly, we would need to calculate how much energy is required to bring the water from 37°C to 100°C (its boiling point):
Energy to heat the water to boiling point (Q1) = mass (m) × specific heat of water (c) × change in temperature (ΔT) = 50 kg × 4180 J/kg·°C × (100°C - 37°C).Afterward, we would need to calculate the energy required to vaporize the water:
Energy to vaporize the water (Q2) = mass (m) × heat of vaporization (Lv) = 50 kg × 2.256×106J/kg.The sum of Q1 and Q2 should be equal to or less than the energy released by the lightning flash for all the water to be vaporized. If there is any excess energy after vaporizing the water, it would further heat the steam. If all the energy is not used in heating and vaporizing the water, the final state would still include some liquid water. A detailed calculation using the provided information and considering the stages involved will give the final temperature and state of the water.
The solar system is 25,000 light years from the center of our Milky Way galaxy. One light year is the distance light travels in one year at a speed of 3.0×108m/s. Astronomers have determined that the solar system is orbiting the center of the galaxy at a speed of 230 km/s.
Answer:
The time period of the solar system's orbit is [tex]2.05\times10^{8}\ year[/tex]
Explanation:
Given that,
Distance = 25000 light year
Speed of light [tex]c=3\times10^{8}\ m/s[/tex]
Speed of astronomers = 230 m/s
Suppose the orbit is circular, we need to find the time period of the solar system's orbit.
We need to calculate the time period
Using formula of time period
[tex]t = \dfrac{d}{v}[/tex]
[tex]t = \dfrac{2\pi r}{v}[/tex]
r = distance
t = time
v = speed
Put the value into the formula
[tex]t=\dfrac{2\pi\times25000\times9.46\times10^{15}}{230\times10^{3}}[/tex]
[tex]t=6.460\times10^{15}\ sec[/tex]
Time in years
[tex]t=\dfrac{6.460\times10^{15}}{3.15\times10^{7}}[/tex]
[tex]t=2.05\times10^{8}\ year[/tex]
Hence, The time period of the solar system's orbit is [tex]2.05\times10^{8}\ year[/tex]
The solar system is about 25,000 light years away from the centre of the Milky Way galaxy. It orbits the galaxy at a speed of 230 km/s, which translates to a galactic year of approximately 225 million Earth years. The galaxy's mass, including dark matter, influences the orbital velocities of all celestial bodies.
Explanation:
The solar system, orbiting at a speed of 230 km/s, is located approximately 25,000 light years from the Milky Way galaxy's center. A light year is defined as the distance light travels in one year with a speed of 3.0×108m/s. Understanding this concept helps us comprehend the vast size of our galaxy. Additionally, the solar system's movement around the Milky Way is referred to as a galactic year, which lasts approximately 225 million years in Earth's time.
The sun, and all stars in the galaxy, orbit the galactic center in a nearly circular path lying in the galaxy's disk. Moreover, the total mass of our Galaxy can be determined by measuring the orbital velocities of stars and interstellar matter, including the Sun. This vast mass, around 2 × 1012 Msun, includes a significant part composed of dark matter that emits no electromagnetic radiation.
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A double-slit interference pattern is observed on a screen 1.0 m behind two slits spaced 0.30 mm apart. From the center of one particular fringe to the center of the ninth bright fringe from this one is 1.6 cm. What is the wavelength of the light? [530nm]
Answer:
The wavelength of the light is 530 nm.
Explanation:
Given that,
Distance D= 1.0 m
Distance between slits d= 0.30 mm
Number of fringe = 9
Width = 1.6 cm
We need to calculate the angle
Using formula of angle
[tex]\tan\theta=\dfrac{y}{D}[/tex]
[tex]tan\theta=\dfrac{1.6\times10^{-2}}{1.0}[/tex]
[tex]\theta=\tan^{-1}(\dfrac{1.6\times10^{-2}}{1.0})[/tex]
[tex]\theta=0.91^{\circ}[/tex]
We need to calculate the wavelength of the light
Using formula of wavelength
[tex]d\sin\theta=m\lambda[/tex]
[tex]\lambda=\dfrac{d\sin\theta}{m}[/tex]
Put the value into the formula
[tex]\lambda= \dfrac{0.30\times10^{-3}\times\sin0.91}{9}[/tex]
[tex]\lambda=5.29\times10^{-7}\ m[/tex]
[tex]\lambda=530\ nm[/tex]
Hence, The wavelength of the light is 530 nm.
Answer:
530 nm
Explanation:
Screen distance, D = 1 m
slit distance, d = 0.3 mm
n = 9 th bright
y = 1.6 cm
Let λ be the wavelength of light used.
y = n x D x λ / d
1.6 x 10^-2 = 9 x 1 x λ / (0.3 x 10^-3)
λ = 5.3333 x 10^-7 m
λ = 533.33 nm
λ = 530 nm ( by rounding off)
A baseball has a mass of 0.15 kg and radius 3.7 cm. In a baseball game, a pitcher throws the ball with a substantial spin so that it moves with an angular speed of 45 rad/s and a linear speed of 42 m/s. Assuming the baseball to be a uniform solid sphere, determine the rotational and translational kinetic energies of the ball in joules.
Answer:
Explanation:
Given
mass of baseball [tex]m=0.15 kg[/tex]
radius of ball [tex]r=3.7 cm[/tex]
angular speed of ball [tex]\omega =45 rad/s[/tex]
linear speed of ball [tex]v=42 m/s[/tex]
Transnational Kinetic Energy is given by
[tex]K.E.=\frac{mv^2}{2}[/tex]
[tex]K.E.=\frac{1}{2}\times 0.15\times 42^2[/tex]
[tex]k.E.=\frac{1}{2}\times 0.15\times 1764[/tex]
[tex] k.E.=132.3 J[/tex]
Considering the ball as solid sphere its moment of inertia is given by
[tex]I=\frac{2}{5}mr^2=\frac{2}{5}\times 0.15\times (0.037)^2[/tex]
[tex]I=8.21\times 10^{-5} kg-m^2[/tex]
Rotational Kinetic Energy
[tex]=\frac{1}{2}\times I\times \omega ^2[/tex]
[tex] =\frac{1}{2}\times 8.21\times 10^{-5}\times 45^2[/tex]
[tex] =\frac{1}{2}\times 8.21\times 10^{-5}\times 2025[/tex]
[tex] =0.0831 J[/tex]
When a 0.350-kg package is attached to a vertical spring and lowered slowly, the spring stretches 12.0 cm. The package is now displaced from its equilibrium position and undergoes simple harmonic oscillations when released. What is the period of the oscillations?
To solve the problem it is necessary to use the concepts related to the calculation of periods by means of a spring constant.
We know that by Hooke's law
[tex]F=kx[/tex]
Where,
k = Spring constant
x = Displacement
Re-arrange to find k,
[tex]k= \frac{F}{x}[/tex]
[tex]k= \frac{mg}{x}[/tex]
[tex]k= \frac{(0.35)(9.8)}{12*10^{-2}}[/tex]
[tex]k = 28.58N/m[/tex]
Perioricity in an elastic body is defined by
[tex]T = 2\pi \sqrt{\frac{m}{k}}[/tex]
Where,
m = Mass
k = Spring constant
[tex]T = 2\pi \sqrt{\frac{0.35}{28.58}}[/tex]
[tex]T = 0.685s[/tex]
Therefore the period of the oscillations is 0.685s
The period of the oscillations can be calculated using the formula T = 2π√(m/k), where m is the mass of the package and k is the spring constant. Plugging in the values mentioned in the question, the period can be determined.
Explanation:The period of the oscillations can be calculated using the formula T = 2π√(m/k), where T is the period, π is a constant (approximately 3.14), m is the mass of the package, and k is the spring constant.
In this case, the mass of the package is 0.350 kg and the spring stretches 12.0 cm (or 0.12 m). The spring constant can be determined using the equation k = mg/X, where g is the acceleration due to gravity (approximately 9.8 m/s2) and X is the displacement (0.12 m).
Plugging the values into the formula, we get T = 2π√(0.350/[(0.350 * 9.8)/0.12]). Solving this equation will give the period of the oscillations.
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A Martian leaves Mars in a spaceship that is heading to Venus. On the way, the spaceship passes earth with a speed v = 0.80c relative to it. Assume that the three planets do not move relative to each other during the trip. The distance between Mars and Venus is 1.20 × 1011 m, as measured by a person on earth. What does the Martian measure for the distance between Mars and Venus?
To find the relative distance from one point to another it is necessary to apply the Relativity equations.
Under the concept of relativity the distance measured from a spatial object is given by the equation
[tex]l = l_0 \sqrt{1-\frac{v^2}{c^2}}[/tex]
Where
[tex]l_0[/tex]= Relative length
v = Velocity of the spaceship
c = Speed of light
Replacing with our values we have that
[tex]l = l_0 \sqrt{1-\frac{v^2}{c^2}}[/tex]
[tex]l = 1.2*10^{11} \sqrt{1-\frac{0.8c^2}{c^2}}[/tex]
[tex]l = 1.2*10^{11} \sqrt{1-0.8^2}[/tex]
[tex]l = 7.2*10^{10}m[/tex]
Therefore the distance between Mars and Venus measured by the Martin is [tex]7.2*10^{10}m[/tex]
A small bolt with a mass of 33.0 g sits on top of a piston. The piston is undergoing simple harmonic motion in the vertical direction with a frequency of 3.05 Hz. What is the maximum amplitude with which the piston can oscillate without the bolt losing contact with the piston's surface? Use g = 9.81 m/s^2 for the acceleration due to gravity.
To determine the maximum amplitude of the piston's oscillation without the bolt losing contact, we need to set the gravitational force equal to the spring force, and solve for the amplitude. Using the given values, including the mass of the bolt, the acceleration due to gravity, and the frequency of oscillation, we can calculate the maximum amplitude.
Explanation:In order for the bolt to stay in contact with the piston's surface, the maximum amplitude of the piston's oscillation needs to be determined.
For simple harmonic motion, the restoring force is proportional to the displacement and acts opposite to the direction of motion. In this case, the restoring force is provided by the weight of the bolt (mg) and the force exerted by the piston (kx), where x is the displacement from equilibrium and k is the spring constant of the piston.
At maximum amplitude, the net force acting on the bolt is zero, so we can set the gravitational force equal to the spring force: mg = kA. Rearranging this equation gives us the maximum amplitude A = mg/k.
Now we can calculate the maximum amplitude using the given values: mass of bolt = 33.0 g = 0.033 kg, acceleration due to gravity g = 9.81 m/s^2, and frequency of oscillation f = 3.05 Hz. The period of oscillation is T = 1/f.
Using the equation T = 2*pi*sqrt(m/k) for the period of a mass-spring system, we can solve for the spring constant k: k = (2*pi/T)^2*m = (2*pi/1/f)^2*0.033 = (2*pi*f)^2*0.033. Plugging in the given value for f, we find k = (2*pi*3.05)^2*0.033.
Finally, we can calculate the maximum amplitude A = mg/k = 0.033*9.81/(2*pi*3.05)^2*0.033. Evaluating this expression gives us the maximum amplitude of the piston's oscillation.
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An arteriole has a radius of 25 μm and it is 1000 μm long. The viscosity of blood is 3 x 10-3 Pa s and its density is 1.055 g cm-3 . Assume the arteriole is a right circular cylinder. A. Assuming laminar flow, what is the resistance of this arteriole?
Answer: [tex]1.955(10)^{13} \frac{Pa.s}{m^{3}}[/tex]
Explanation:
This can be solved by the Poiseuille’s law for a laminar flow:
[tex]R=\frac{8 \eta L}{\pi r^{4}}[/tex]
Where:
[tex]R[/tex] is the resistance of the arteriole
[tex]\eta=3(10)^{-3} Pa.s[/tex] is the viscosity of blood
[tex]L=1000 \mu m=1000(10)^{-6}m[/tex] is the length of the arteriole
[tex]r=25 \mu m=25(10)^{-6}m[/tex] is the radius of the arteriole
[tex]R=\frac{8 (3(10)^{-3} Pa.s)(1000(10)^{-6}m)}{\pi (25(10)^{-6}m)^{4}}[/tex]
[tex]R=1.955(10)^{13} \frac{Pa.s}{m^{3}}[/tex]
The resistance of the arteriole is calculated using the Hagen-Poiseuille equation, resulting in an approximate value of 1.96 × 10¹⁵ Pa·s·m⁻⁴. The formula determines resistance by varying viscosity, length, and radius values, which is essential for understanding blood flow dynamics in physiological settings.
We can solve this problem using the formula for fluid resistance in a cylindrical tube (Hagen-Poiseuille equation):
[tex]R = (8 \times \eta \times L) / (\pi \times r_4)[/tex]
Where:
R is the resistance.η is the viscosity of the fluid (3 × 10⁻³ Pa·s).L is the length of the tube (1000 × 10⁻⁶ m).r is the radius of the tube (25 × 10⁻⁶ m).Substituting the values:
[tex]R = (8 \times 3 \times 10^{-3} Pa\cdot s \times 1000 \times 10^{-6} m) / (\pi \times (25 \times 10^{-6} m))[/tex]
Calculating the values inside the formula:
[tex]R = (24 \times 10^{-3} Pa\cdot s\cdot m) / (\pi \times 3.90625 \times 10^{-18} m^{4})[/tex][tex]R = (24 \times 10^{-3} Pa\cdot s\cdot m) / (1.227 \times 10^{-17} m^{4})[/tex][tex]R \approx 1.96 \times 1015 Pa\cdot s/m^{-4}[/tex]So, the resistance of the arteriole is approximately 1.96 × 10¹⁵ Pa·s·m⁻⁴.
You go to the hardware store to buy a new 50 ft garden hose. You find you can choose between hoses of ½ inch and 5/8 inch inner diameter. Compared the rate at which water flows through the two types of hoses (i.e. the ratio of rates).
To solve this problem it is necessary to consider two concepts. The first of these is the flow rate that can be defined as the volumetric quantity that a channel travels in a given time. The flow rate can also be calculated from the Area and speed, that is,
Q = V*A
Where,
A= Cross-sectional Area
V = Velocity
The second concept related to the calculation of this problem is continuity, which is defined as the proportion that exists between the input channel and the output channel. It is understood as well as the geometric section of entry and exit, defined as,
[tex]Q_1 = Q_2[/tex]
[tex]V_1A_1=V_2A_2[/tex]
Our values are given as,
[tex]A_1=\frac{1}{2}^2*\pi=0.785 in^2[/tex]
[tex]A_2=\frac{5}{8}^2*\pi=1.227 in^2[/tex]
Re-arrange the equation to find the first ratio of rates we have:
[tex]\frac{V_1}{V_2}=\frac{A_2}{A_1}[/tex]
[tex]\frac{V_1}{V_2}=\frac{1.227}{0.785}[/tex]
[tex]\frac{V_1}{V_2}=1.56[/tex]
The second ratio of rates is
[tex]\frac{V2}{V1}=\frac{A_1}{A2}[/tex]
[tex]\frac{V2}{V1}=\frac{0.785}{1.227}[/tex]
[tex]\frac{V2}{V1}=0.640[/tex]
The ratio of the flow rate of a ½ inch hose to that of a 5/8 inch hose is 16:25. This means that under equal pressures, for every 16 gallons of water that pass through the ½ inch hose, 25 gallons could flow through the 5/8 inch hose.
Explanation:To compare the flow rates within the two hoses, we'll utilize a principle of fluid dynamics which states that the flow rate of an incompressible fluid (like water) is proportional to the cross-sectional area of the pipe. The area can be calculated using the formula for the area of a circle: A=πr², where r is the radius of the pipe.
To transform the diameters into radii, we divide them by 2: the radii are therefore 1/4 inch and 5/16 inch. As we're primarily interested in the ratio of areas (and consequently flow rates), we can ignore the π in the equation, leaving us with r² as directly representing 'area' for this comparison.
(1/4)² = 1/16 and (5/16)² = 25/256. Hence, the flow rate of the ½-inch hose to the 5/8 inch hose is 1/16: 25/256.
To simplify, we can multiply both portions of the ratio by 256 to achieve 16:25. This means for every 16 gallons per minute through the ½ inch hose, 25 gallons per minute could flow through the 5/8-inch hose, assuming the pressure in both systems is equal.
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Part A
Calculate the magnitude of the maximum orbital angular momentum Lmax for an electron in a hydrogen atom for states with a principal quantum number of 7.
Express your answer in units of ℏ to three significant figures.
Part B
Calculate the magnitude of the maximum orbital angular momentum Lmax for an electron in a hydrogen atom for states with a principal quantum number of 26.
Express your answer in units of ℏ to three significant figures.
Part C
Calculate the magnitude of the maximum orbital angular momentum Lmax for an electron in a hydrogen atom for states with a principal quantum number of 191.
Express your answer in units of ℏ to three significant figures.
Answer:
Explanation:
A )
[tex]L_{max} = \sqrt{l(l+1)}[/tex]ℏ
where l is orbital quantum number
l = n-1 where n is principal quantum no
Given n = 7
l = 7 - 1 = 6
[tex]L_{max} = \sqrt{6(6+1)}[/tex]ℏ
= 6.48ℏ
B)
Here
n = 26
l = 26 - 1
= 25
[tex]L_{max} = \sqrt{25(25+1)}[/tex]ℏ
= 25.49ℏ
= 25.5ℏ
C )
n = 191
l = 191 - 1
190
[tex]L_{max} = \sqrt{190(190+1)}[/tex]
= 190.499ℏ
= 191ℏ
The magnitude of the maximum orbital angular momentum Lmax for an electron in a hydrogen atom can be calculated using the formula Lmax = √(l*(l + 1)), where l is the orbital quantum number, which for maximum Lmax is n - 1 for principal quantum number n. The values for n = 7, 26, and 191 are approximately 16.9706 ℏ, 81.6144 ℏ, and 675.3918 ℏ, respectively.
Explanation:The magnitude of the maximum orbital angular momentum for an electron in a hydrogen atom can be expressed in terms of the principal quantum number n. The maximum value of the orbital quantum number, l, is n - 1.
The magnitude of the maximum orbital angular momentum Lmax is then given by the square root of l*(l + 1). Therefore:
For a principal quantum number n = 7, l = 7 - 1 = 6. Consequently, Lmax = √(l*(l + 1)) = √(6*7) = 16.9706 ℏ to three significant figures. For a principal quantum number n = 26, l = 26 - 1 = 25. Consequently, Lmax = √(l*(l + 1)) = √(25*26) = 81.6144 ℏ to three significant figures.For a principal quantum number n = 191, l = 191 - 1 = 190. Consequently, Lmax = √(l*(l + 1)) = √(190*191) = 675.3918 ℏ to three significant figures. Learn more about Orbital Angular Momentum here:https://brainly.com/question/35912005
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we must apply a force of magnitude 83 N to hold the block stationary at x = −2.0 cm. From that position we then slowly move the block so that our force does +4.8 J of work on the spring-block system; the block is then again stationary. What is the block's position x? (There are two answers.)
The concept required to develop this problem is Hook's Law and potential elastic energy.
By definition the force by Hooke's law is defined as
[tex]F = kx[/tex]
Where,
k = Spring Constant
x = Displacement
On the other hand, the elastic potential energy is defined as
[tex]E = \frac{1}{2} k\Delta x^2[/tex]
With the given values we can find the value of the spring constant, that is,
[tex]F = kx[/tex]
[tex]k=\frac{F}{x}[/tex]
[tex]k= \frac{83}{0.02}[/tex]
[tex]k = 4120N/m[/tex]
Applying the concepts of energy conservation then we can find the position of the block, that is,
[tex]E = \frac{1}{2} k\Delta x^2[/tex]
[tex]E = \frac{1}{2} k\Delta x^2[/tex]
[tex]4.8 = \frac{1}{2} (4120)(x^2-(-0.02)^2)[/tex]
[tex]x = \sqrt{\frac{2*4.8}{4120}+(-0.02)^2}[/tex]
[tex]x = \pm 0.05225m[/tex]
Therefore the position of the block can be then,
[tex]x_1 = 5.225cm[/tex]
[tex]x_2 = -5.225cm[/tex]
A large fraction of the ultraviolet (UV) radiation coming from the sun is absorbed by the atmosphere. The main UV absorber in our atmosphere is ozone, O3. In particular, ozone absorbs radiation with frequencies around 9.38×1014 Hz . What is the wavelength λ of the radiation absorbed by ozone?
Answer:
[tex]\lambda=3.20*10^{-7}m[/tex]
Explanation:
The wavelength is inversely proportional to the frequency. The wavelength is equal to the speed of the wave, divided by the frequency. In the case of electromagnetic waves like ultraviolet radiation, the speed of propagation is the speed of light.
[tex]\lambda=\frac{c}{f}\\\lambda=\frac{3*10^8\frac{m}{s}}{9.38*10^{14}Hz}\\\lambda=3.20*10^{-7}m[/tex]
Answer : The wavelength of the radiation absorbed by ozone is, [tex]3.20\times 10^{-7}m[/tex]
Explanation : Given,
Frequency = [tex]9.38\times 10^{14}Hz=9.38\times 10^{14}s^{-1}[/tex]
Formula used :
[tex]\nu=\frac{c}{\lambda}[/tex]
where,
[tex]\nu[/tex] = frequency
[tex]\lambda[/tex] = wavelength
c = speed of light = [tex]3\times 10^8m/s[/tex]
Now put all the given values in the above formula, we get:
[tex]9.38\times 10^{14}s^{-1}=\frac{3\times 10^8m/s}{\lambda}[/tex]
[tex]\lambda=3.20\times 10^{-7}m[/tex]
Therefore, the wavelength of the radiation absorbed by ozone is, [tex]3.20\times 10^{-7}m[/tex]
A mouse is running along the floor in a straight line at 1.3 m/s. A cat runs after it and, perfectly judging the distance d to the mouse ahead, springs up at a speed of 2.5 m/s and an angle 38 degree, landing right on top of the mouse.
What is d, the distance between the cat and mouse at the instant the cat springs into the air?
a)0.931 m
b)0.210 m
c) 0.401 m
d)0.552 m
e)0.641m
Answer:
Option b
Solution:
As per the question:
Speed of the mouse, v = 1.3 m/s
Speed of the cat, v' = 2.5 m/s
Angle, [tex]\theta = 38^{\circ}[/tex]
Now,
To calculate the distance between the mouse and the cat:
The distance that the cat moved is given by:
[tex]x = v'cos\theta t[/tex]
[tex]x = 2.5cos38^{\circ}\times t = 1.97t[/tex]
The position of the cat and the mouse can be given by:
[tex]x = x' + vt[/tex]
[tex]1.97t = x' + 1.3t[/tex]
x' = 0.67 t (1)
The initial speed of the cat ahead of the mouse:
u = [tex]v'sin\theta = 2.5sin38^{\circ} = 1.539\ m/s[/tex]
When the time is 0.5t, the speed of the cat is 0, thus:
[tex]0 = u - 0.5tg[/tex]
[tex]t = \frac{1.539}{0.5\times 9.8} = 0.314\ s[/tex]
Substituting the value of t in eqn (1):
x' = 0.67(0.314) = 0.210 m
Thus the distance comes out to be 0.210 m
A small artery has a length of 1.10 × 10 − 3 m and a radius of 2.50 × 10 − 5 m. If the pressure drop across the artery is 1.45 kPa,what is the flow rate through the artery? Assume that the temperature is 37 °C and the viscosity of whole blood is 2.084 × 10 − 3 Pa·s.
Answer:
The flow rate is [tex]9.7\times 10^{- 11}\ m^{3}/s[/tex]
Solution:
As per the question:
Pressure drop, = 1.45 kPa = 1450 Pa
Radius of the artery, R = [tex]2.50\times 10^{- 5}\ m[/tex]
length of the artery, L = [tex]1.10\times 10^{- 3}\ m[/tex]
Temperature, T = [tex]37^{\circ}C[/tex]
Viscosity, [tex]\eta = 2.084\times 10^{- 3}\ Pa.s[/tex]
Now,
The flow rate is given by:
[tex]Q = \frac{\pi R^{4}P}{8\eta L}[/tex]
[tex]Q = \frac{\pi (2.50\times 10^{- 5})^{4}\times 1450}{8\times 2.084\times 10^{- 3}\times 1.10\times 10^{- 3}} = 9.7\times 10^{- 11}\ m^{3}/s[/tex]
The flow rate through the artery can be calculated using Poiseuille's law, which takes into account the pressure difference, radius, length, and viscosity of the fluid. Using the given values, the flow rate is approximately 0.00686 m^3/s.
Explanation:The flow rate through an artery can be calculated using Poiseuille's law, which states that the flow rate is directly proportional to the pressure difference and the fourth power of the radius, and inversely proportional to the length and viscosity of the fluid.
Using the given values, we can calculate the flow rate as follows:
Flow rate = (pressure difference * pi * radius^4) / (8 * viscosity * length)
Substituting the given values into the equation gives:
Flow rate = (1.45 * 10^3 * 3.14 * (2.5 * 10^-5)^4) / (8 * 2.084 * 10^-3 * 1.10 * 10^-3) = 0.00686 m^3/s
Therefore, the flow rate through the artery is approximately 0.00686 m^3/s.
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The density of the liquid flowing through a horizontal pipe is 1200 kg/m3. The speed of the fluid at point A is 7.5 m/s while at point B it is 11 m/s. What is the difference in pressure, PB – PA, between points B and A?A. +5.0 × 104 PaB. –1.9 × 103 PaC. –2.5 × 104 PaD. –3.9 × 104 PaE. +3.8 × 103 Pa
Answer:
The difference in pressure between points B and A is [tex]-3.9\times10^{4}\ Pa[/tex]
(D) is correct option.
Explanation:
Given that,
Density of the liquid = 1200 kg/m³
Speed of fluid at point A= 7.5 m/s
Speed of fluid at point B = 11 m/s
We need to calculate the difference in pressure between points B and A
Using formula of change in pressure
[tex]\Delta P=\dfrac{1}{2}D(v_{2}^2-v_{1}^2)[/tex]
Where, [tex]v_{1}[/tex] = Speed of fluid at point A
[tex]v_{2}[/tex] = Speed of fluid at point B
D = Density of the liquid
Put the value into the formula
[tex]\Delta P=\dfrac{1}{2}\times1200\times(11^2-7.5^2)[/tex]
[tex]\Delta P=-38850\ Pa[/tex]
[tex]\Delta P=-3.9\times10^{4}\ Pa[/tex]
Hence, The difference in pressure between points B and A is [tex]-3.9\times10^{4}\ Pa[/tex]
The difference in pressure, PB – PA, between points B and A can be calculated using Bernoulli's equation. Plugging in the given values, we find that the pressure difference is approximately -39,000 Pa.
Explanation:
The difference in pressure between points B and A can be calculated using Bernoulli's equation. Bernoulli's equation states that the pressure difference between two points in a fluid flow system is equal to the difference in kinetic energy and potential energy between the two points. In this case, we can calculate the pressure difference using the equation:
PB - PA = (1/2) * ρ * (VB^2 - VA^2)
PB - PA = (1/2) * 1200 kg/m3 * (11 m/s)^2 - (7.5 m/s)^2
Simplifying the equation, we find that the difference in pressure, PB - PA, is approximately -39,000 Pa. Therefore, the correct answer is D. -3.9 × 104 Pa.
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