Fill in the blanks: the standard international (SI) unit for mass is the , The standard international (SI) unit for force is the .

The current flowing over the 30 Ω resistor is 0.4 A.

To discover the current streaming over the 30 Ohm resistor, able to apply Ohm's Law, which states that the current (I) is break even with to the voltage (V) partitioned by the resistance (R). In this case, the voltage over the circuit is given as 9.0 V.

To calculate the full resistance of the circuit, we ought to consider the resistors in arrangement and parallel. The resistors with values of 40 Ω and 50 Ω are in serie.

Hence, the sum of their value (R_series )= 40 Ω + 50 Ω = 90 Ω. The 20 Ω and 10 Ω resistors are in parallel, hence, their resistance is represented as (1/R_parallel) = 1/20 Ω + 1/10 Ω = 1/10 Ω. Disentangling this expression gives R_parallel = 6.67 Ω.

Presently, ready to calculate the entire resistance of the circuit. The resistors with values of 30 Ω and 90 Ω (from the arrangement combination) are in parallel, so their identical resistance is given by 1/R_total = 1/30 Ω + 1/90 Ω = 1/22.5 Ω. Rearranging this expression gives R_total = 22.5 Ω.

At last, able to apply Ohm's Law to discover the current over the 30 Ω resistor. I = V / R_total = 9.0 V / 22.5 Ω ≈ 0.4 A.

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Ohm's law is defined as the applied voltage (V) is directly proportional to the current flow (I) in the circuit. V =IR, where R is the resistance of the circuit that resists the current flow in the circuit, and the unit of resistance is the ohm.

From the given,

1) a) resistors in the circuit are connected in parallel, then the voltage in the circuit remains the same. The voltage across each resistor is 9V.

  b) the current in each resistor is given by, V=IR

I₁ = V/R₁ = 9/10kΩ=0.9mA.

I₂ = V/R₂ = 9/2kΩ = 4.5mA

I₃ = V/R₃ = 9/1kΩ = 9mA.

2) a) the resistances are connected in parallel, the effective resistance is 1/R(eff) = 1/R₁ + 1/R₂

1/R(eff) = 1/(100) + 1/(250)

           = 250+100/25000

          = 350/25000

          = 7/500

R₁(eff) = 500/7

1/R(eff) = 1/R₁ + 1/R₂

            = 1/350 + 1/200

            = 200+350/70000

            = 550/70000

            = 11/1400

R₂(eff) = 1400/11

Thus, the two effective resistances are connected in series,

R(e) = R₁(eff) + R₂(eff)

      = 500/7 + 1400/11

      = (500×11) + (1400×7)/77

      = 5500 + 9800 / 77

      = 15300/77

R(e) = 198 Ω.

B) total current, I = V/R

  I = 24 /198

   = 121mA.

3) a) the resistances are connected in series, the total resistance,

R(eff) = R₁ + R₂

         = 3+3

R(eff) = 6Ω

b)Current, I = V/R

I = 12/6

  = 2A

c)Power, P = I²R = 2×2×6

      P = 24W is the power in each bulb.

d) Power, P = VI = 12×2 = 24 W, is the power in battery.

4) a) the resistances are connected in parallel,

1/R(eff) = 1/R₁ + 1/R₂

           = 1/3 + 1/3

           = 2/3

R(eff) = 3/2Ω

b) In a parallel circuit, the voltage remains unchanged.

Voltage = 12V

c) Current, I = V/R

I₁ = V/R₁ = 12/3 = 4A

I₂ = V/R₂ = 12/3 = 4A.

d) power, P = I²R =4²3=48W.

e) Total current in the circuit, I = I₁+I₂

I = 4 + 4

 = 8A

f) power supplied by a battery, P = VI

P = 12×4 = 48 W.

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a) Converting the time interval to hours is 0.2 hr

b) The time in seconds is 691468 sec

To determine the time interval during which the rockets must be fired, we can analyze the forces acting on the ring. The rockets provide a tangential force that causes the ring to rotate. This force creates a torque, which results in an angular acceleration. To maintain an effective free-fall acceleration equal to g, the angular acceleration should be equal to g divided by the radius of the ring.

(a) To calculate the time interval, we can use the equation:

θ = ω_i * t + (1/2) * α * t^2

where θ is the angle through which the ring rotates, ω_i is the initial angular velocity, α is the angular acceleration, and t is the time interval. Since the ring starts from rest, ω_i = 0.

The angle θ is given by:

θ = 2π

The angular acceleration α can be calculated using:

α = g / r

where g is the acceleration due to gravity and r is the radius of the ring.

Substituting the given values, we have:

2π = (1/2) * (g / r) * t^2

Solving for t, we get:

t = sqrt((4πr) / g)

Converting the time interval to hours, we divide by 3600:

t = sqrt((4πr) / g) / 3600= 0.2 hr

(b) The period of rotation can be calculated using the equation:

T = 2π / ω

where T is the period and ω is the angular velocity.

Since the angular velocity ω is related to the angular acceleration α by the equation:

ω = α * t

Substituting the values, we have:

T = 2π / (α * t)

Substituting the values of α and t, we get:

T = 2π / (g / r * sqrt((4πr) / g) / 3600)

Simplifying the expression, we have:

T = (2π * r * 3600) / sqrt(4πr * g)= 691468 sec

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a.  output voltage is 110 V, the RMS output voltage is approximately 155.56 V, the output (load) current is 15.56 A, the ripple factor is 0.866, and the form factor is 0.866. b. the input active power is 2640 W, the input apparent power is 2640 VA, and the power factor is 1 (or unity).

a. For a single-phase full-bridge uncontrolled (diode) rectifier with a pure resistive load of R = 10 Ohms and neglecting diode volt-drops, we can calculate the following values:

Average Output Voltage:

The average output voltage of a full-bridge rectifier can be calculated as half of the peak input voltage. Since the input voltage is 220 V, the average output voltage will be:

Average Output Voltage = (220 V) / 2 = 110 V

RMS Output Voltage:

The RMS output voltage of a full-bridge rectifier can be calculated as the peak input voltage divided by the square root of 2. In this case, the RMS output voltage will be:

RMS Output Voltage = (220 V) / √2 ≈ 155.56 V

Output (Load) Current:

Since the load is pure resistive, the output (load) current will be the same as the RMS output voltage divided by the load resistance. Therefore:

Output (Load) Current = RMS Output Voltage / R = 155.56 V / 10 Ω = 15.56 A

Ripple Factor:

The ripple factor for a full-bridge rectifier can be calculated as the ratio of the RMS value of the ripple voltage to the average output voltage. In this case, since we are neglecting diode volt-drops, the ripple factor is:

Ripple Factor = √(3/4) ≈ 0.866

Form Factor:

The form factor is the ratio of the RMS value of the output current to its average value. Since the load is purely resistive, the form factor is the same as the ripple factor:

Form Factor = 0.866

b. Now, assuming the load has an inductive nature with L >> R and a load current of 12 Amperes:

Input Active Power:

The input active power can be calculated as the product of the RMS input voltage, RMS input current, and the power factor. In this case, since the load current is flat and equal to 12 Amperes, and we neglect diode losses, the input active power will be:

Input Active Power = (220 V) * (12 A) = 2640 W

Input Apparent Power:

The input apparent power can be calculated as the product of the RMS input voltage and RMS input current. Therefore:

Input Apparent Power = (220 V) * (12 A) = 2640 VA

Power Factor:

The power factor is the ratio of the input active power to the input apparent power. In this case, the power factor will be:

Power Factor = Input Active Power / Input Apparent Power = 2640 W / 2640 VA = 1 (or unity)

Note: Neglecting diode losses implies that we assume the diodes are ideal, without any voltage drops or losses during the rectification process. In practical scenarios, there will be some voltage drops across the diodes, and losses should be taken into account for more accurate calculations.

Therefore, a. For a single-phase full-bridge uncontrolled (diode) rectifier with a pure resistive load of 10 Ohms, neglecting diode volt-drops, the average output voltage is 110 V, the RMS output voltage is approximately 155.56 V, the output (load) current is 15.56 A, the ripple factor is 0.866, and the form factor is 0.866. b. Assuming a load with an inductive nature, L >> R, and a flat load current of 12 A, the input active power is 2640 W, the input apparent power is 2640 VA, and the power factor is 1 (or unity).

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According to the diagram the equivalent resistance of the group is

40.05 ohms

The equivalent resistance is calculated by investigating the diagram to note that R2 and R3 are in parallel and both are in series to R1

Resistors in parallel is solved by

Resistors in parallel = 1/25.4 + 1/70.8

Resistors in parallel = 0.0535 ohms

Equivalent resistance

Equivalent resistance = Resistors in parallel + Resistor in series

Equivalent resistance = 0.0535 + 40

Equivalent resistance = 40.0535

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Plasma lacks a precise form or volume, much like gas. It completes the empty space. Even though it is in the gaseous form, there is a difference because some of the particles are plasma-ionized.

High-energy particles are free to move around and fill the area they inhabit in the state of matter known as gas.

Neutral atoms or molecules often make up gaseous substances like air.

The ionised gas known as plasma, on the other hand, contains both positively and negatively charged particles.

It develops when a gas is subjected to an intense electric field or heated to incredibly high temperatures.

Plasma is a substance that may be found in stars, lightning, and fluorescent lights. It is also an essential component of many modern technology, like plasma TVs and fusion reactors.

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Answer:

3 : Presence of a catalyst and Temperature

4 : correct, nothing needed to change

5 : Le Chatelier's principle states that when an equilibrium system is subjected to a disturbance or stress, it will undergo a shift in the direction that counteracts the impact of the stress, ultimately reestablishing a new state of equilibrium.

Answer:

4000 Nm^-2

Explanation:

Dude that "zam" drove me away, anyway:

Given:

Force on the large piston (F1) = 4000 N

Cross-sectional area of the large piston (A1) = 1 m²

Cross-sectional area of the small piston (A2) = zam (let's assume zam represents the area in square meters)

According to Pascal's law, the pressure exerted on the large piston (P1) is equal to the pressure exerted on the small piston (P2):

P1 = P2

Pressure is defined as force divided by area:

P1 = F1 / A1

P2 = F2 / A2

Since P1 = P2, we can equate the two expressions:

F1 / A1 = F2 / A2

Rearranging the equation to solve for F2, the force on the small piston:

F2 = (F1 / A1) * A2

Substituting the given values:

F2 = (4000 N / 1 m²) * zam

Now, to calculate the pressure exerted on the small piston (P2), we can divide the force by the area:

P2 = F2 / A2

Substituting the values we obtained:

P2 = [(4000 N / 1 m²) * zam] / zam

The area "zam" cancels out in the equation, leaving us with:

P2 = 4000 N/m²

Therefore, the pressure exerted on the small piston is 4000 N/m².

To determine the effort required on the small piston, we need to know the area of the small piston. Once we have that information, we can substitute it into the equation for F2 to calculate the effort required

Answer:

both objects are negatively charged.

The total distance covered by the car is 300 miles.

The total displacement covered by the car is zero.

The average speed of the car is 17.88 m/s.

The average velocity of the car is also zero.

Distance between the points A and B, d = 150 miles

Time taken by the car to travel from A to B, t₁ = 3 hours

Time taken by the car to travel from B to A, t₂ = 5 hours

a) Given that the car travelled from A to B and then back to A.

Therefore, the total distance covered by the car is,

Distance = 2 x d

Distance = 2 x 150

Distance = 300 miles

Since the car is travelling from A to B and then returning back to the initial point A, the total displacement covered by the car is zero.

b) The speed with which the car travelled from A to B is,

v₁ = d/t₁

v₁ = 150/3

v₁ = 50 miles/hr

v₁ = 22.35 m/s

The speed with which the car travelled from B to A is,

v₂ = d/t₂

v₂ = 150/5

v₂ = 30 miles/hr

v₂ = 13.41 m/s

Therefore, the average speed of the car is,

v = (v₁ + v₂)/2

v = (22.35 + 13.41)/2

v = 17.88 m/s

As, the total displacement of the car is zero, the average velocity of the car is also zero.

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The correct statements are:Charge Q is positive, the electric field is nonuniform and if charge A is negative, it moves away from charge Q.

Based on the given information, we can make the following conclusions:

Charge Q is positive: The diagram shows that the electric field vectors point radially inward towards charge Q. Since like charges repel each other, for the vectors to point towards charge Q, it must be positive.

The electric field is nonuniform: The statement mentions that "the farther you get from the charge, the shorter the vectors." This implies that the magnitude of the electric field decreases with distance from charge Q. Therefore, the electric field is nonuniform.If charge A is negative, it moves away from charge Q: In the diagram, charge A is within the electric field of charge Q. Since opposite charges attract each other, if charge A is negative, it will experience a force that pulls it towards charge Q. Therefore, it will move towards charge Q, not away from it.

If charge A is positive, it moves away from charge Q: This statement is incorrect. According to the previous conclusion, if charge A is positive, it will experience a force that attracts it towards charge Q. Therefore, it will move towards charge Q, not away from it.

The provided information does not specify the behavior of charge A when it is positive. It is possible that charge A could move towards charge Q, or it could experience other forces depending on its position and the magnitude of the charges involved.

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The initial temperature of the cold water is 10°C.

Mass of the cold water, m₁ = 400 g = 0.4 g

Mass of the water to which the cold water is added, m₂ = 200 g = 0.2 g

Temperature of the water to which the cold water is added, T₂ = 70°C

Temperature of the mixture, T = 30°C

According to the principle of calorimetry,

m₁T₁ + m₂T₂ = (m₁ + m₂)T

(0.4 x T₁) + (0.2 x 70) = (0.4 + 0.2) x 30

0.4T₁ + 14 = 18

0.4T₁ = 18 - 14

0.4T₁ = 4

Therefore, the initial temperature of the cold water is,

T₁ = 4/0.4

T₁ = 10°C

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The third-largest continent, North America, with an area of 24,346,000 sq km.

Thus, The entire continent of North America, including any associated offshore islands, is located north of the Panama Canal, which connects it to South America.

It features a wide range of climates, from the sweltering heat of the tropics to the dry, icy cold of the Arctic. An icecap is always there, keeping the interior of Greenland permanently cold and climate.

Only briefly each summer do temperatures above zero degrees Fahrenheit rise in the vast, treeless tundra of North America. Low-lying regions in the deep south are constantly hot and wet. The majority of the rest of North America experiences chilly winters and mild summers.

Thus, The third-largest continent, North America, with an area of 24,346,000 sq km.

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The increase in length of the iron wire when warmed from 20°C to 45°C is approximately 8.25 millimeters. The specific heat capacity of the object is approximately 9.62 J/kg°C. The heat capacity of the object is approximately 1.83 J/°C.

ΔL = L × α × ΔT

Where:

ΔL is the change in length

L is the original length of the wire

α is the coefficient of linear expansion for iron

ΔT is the change in temperature

The coefficient of linear expansion for iron is typically 1.1 x [tex]10^(^-^5^)[/tex] °[tex]C^(^-^1^)[/tex].

Given:

L = 30 m (original length of the wire)

α = 1.1 x [tex]10^(^-^5^)[/tex] °[tex]C^(^-^1^)[/tex] (coefficient of linear expansion)

ΔT = 45°C - 20°C = 25°C (change in temperature)

ΔL = 30 m × (1.1 x [tex]10^(^-^5^)[/tex] °[tex]C^(^-^1^)[/tex]) × 25°C

= 30 m × 1.1 x[tex]10^(^-^5^)[/tex] × 25

= 8.25 x [tex]10^(^-^3^)[/tex] m

2) Q = mcΔT

Where:

Q is the heat energy transferred

m is the mass of the object

c is the specific heat capacity

ΔT is the change in temperature

Given:

Q = 2200 J (heat energy transferred)

m = 190 g (mass of the object)

ΔT = 12°C (change in temperature)

a. Specific heat capacity (c):

one need to rearrange the formula to solve for c:

c = Q / (m × ΔT)

Substituting the given values:

c = 2200 J / (190 g × 12°C)

First, need to convert the mass to kilograms:

m = 190 g = 190 g / 1000 = 0.19 kg

Now can calculate the specific heat capacity:

c = 2200 J / (0.19 kg × 12°C)

= 9.62 J/(kg°C)

b. Heat capacity (C):

The heat capacity is the amount of heat energy required to raise the temperature of the object by 1 degree Celsius.

C = mc

Substituting the given values:

C = 0.19 kg × 9.62 J/(kg°C)

= 1.83 J/°C

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The resistance of the second wire is twice the resistance of the first wire R₂ = 2R₁

The resistance of a wire is directly proportional to its length and inversely proportional to the cross-sectional area.

Let:

R₁ = resistance of the first wire

R₂ = resistance of the second wire

L₁ = length of the first wire

L₂ = length of the second wire

r₁ = radius of the first wire

r₂ = radius of the second wire

Given:

L₂ = L₁/2

r₂ = r₁/2

A₂ = A₁/4

Since resistance is inversely proportional to the cross-sectional area, which is proportional to the square of the radius.

Now, we can use the formula for resistance:

R = (ρL) / A

where

ρ is the resistivity,

L is the length,  

A is the cross-sectional area.

For the first wire:

R₁ = (ρL₁) / A₁

For the second wire:

R₂ = (ρL₂) / A₂

Substituting the relationships we derived earlier:

R₂ = (ρ(L₁/2)) / (A₁/4)

R₂ = (ρL₁) / (A₁/2)

R₂ = 2(ρL₁) / A₁

Since ρL₁/A₁ is equal to R₁ (the resistance of the first wire), we can substitute:

R₂ = 2R₁

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Answer:

The difference between (a) and (b) is the deviation caused by the actual pulley not being a perfect solid disk. In (a), we took into account the additional frictional torque and calculated the more accurate moment of inertia. In (b), we made a rough estimate assuming the pulley to be a solid disk, which disregards factors such as the mass distribution and the presence of the axle. The difference between the two values is the deviation caused by these factors.

The magnitude of the maximum velocity of the mass is 1.43 m/s.

The maximum velocity of the mass will occur when it is at the equilibrium point. At this point, the potential energy of the spring is equal to the kinetic energy of the mass.

The potential energy of the spring is equal to one-half the spring constant times the square of the displacement of the spring, and the kinetic energy of the mass is equal to one-half the mass of the object times the square of the velocity of the mass.

We are given that the spring constant is 11.7 N/m, the displacement of the spring is 0.194 m, and the mass of the object is 0.402 kg. Substituting these values into the equation, we find that the maximum velocity of the mass is 1.43 m/s.

Therefore, the magnitude of the maximum velocity of the mass is 1.43 m/s.

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Answer:

Yes, the shark's weight or mass is what causes the bottom string to break. The weight of the shark creates tension on the bottom string, which can cause it to snap if the tension becomes too great.

1. The angular momentum of the combined bullet-block system about the vertical pivot axis is 0.

2. The fraction of the original kinetic energy of the bullet converted into internal energy within the bullet-block system during the collision is given by [m * v² - (M + m) * V²] / [m * v²].

1. To find the angular momentum of the combined bullet-block system about the vertical pivot axis, we need to consider the initial and final angular momentum.

Initially, before the collision, the bullet has no angular momentum about the pivot axis since it is moving parallel to the table and perpendicular to the rod.

After the collision, when the bullet embeds within the block, the combined bullet-block system starts rotating about the pivot axis due to the conservation of angular momentum.

The angular momentum of the system can be calculated using the formula:

Angular momentum = moment of inertia × angular velocity

The moment of inertia of the system depends on the distribution of mass and the axis of rotation. Assuming the block and bullet have negligible rotational inertia compared to the rod, we can consider the moment of inertia to be that of the rod.

The moment of inertia of a rod rotating about one end (pivot) is given by:

I = (1/3) * M * ℓ²

where M is the mass of the block, and ℓ is the length of the rod.

The angular velocity (ω) can be determined by considering the conservation of angular momentum:

Initial angular momentum = Final angular momentum

0 = (1/3) * M * ℓ² * ω

Since the initial angular momentum is zero, the final angular momentum of the system is also zero.

Therefore, the angular momentum of the combined bullet-block system about the vertical pivot axis is 0.

2. To find the fraction of the original kinetic energy of the bullet that is converted into internal energy within the bullet-block system during the collision, we can use the principle of conservation of kinetic energy.

The initial kinetic energy of the bullet before the collision is given by:

Initial kinetic energy = (1/2) * m * v²

After the collision, the bullet embeds within the block, and both the bullet and the block gain internal kinetic energy due to their rotational motion.

The final kinetic energy of the bullet-block system is given by:

Final kinetic energy = (1/2) * (M + m) * V²

where V is the final velocity of the combined bullet-block system after the collision.

Since the bullet and block are now rotating about the pivot axis, part of the initial kinetic energy is converted into internal rotational kinetic energy.

The fraction of the original kinetic energy converted into internal energy can be calculated as:

Fraction of kinetic energy converted = (Initial kinetic energy - Final kinetic energy) / Initial kinetic energy

Substituting the values:

Fraction of kinetic energy converted = [(1/2) * m * v² - (1/2) * (M + m) * V²] / [(1/2) * m * v²]

Simplifying the equation, we can cancel out common terms:

Fraction of kinetic energy converted = [m * v² - (M + m) * V²] / [m * v²]

Therefore, the fraction of the original kinetic energy of the bullet converted into internal energy within the bullet-block system during the collision is given by [m * v² - (M + m) * V²] / [m * v²].

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The strength of gravity on the moon is approximately 1.6 J/kg.

The change in gravitational potential energy (GPE) is given by the equation:

ΔGPE = m * g * Δh

where ΔGPE is the change in gravitational potential energy, m is the mass of the object, g is the strength of gravity, and Δh is the change in height.

In this case, the astronaut's GPE increases by 880 J as he climbs up the ladder by 5 m. We can rewrite the equation as:

880 J = (110 kg) * g * (5 m)

To find the strength of gravity on the moon (g), we can rearrange the equation:

g = 880 J / (110 kg * 5 m)

g = 1.6 J/kg

Therefore, the strength of gravity on the moon is approximately 1.6 J/kg.

It's important to note that the value of gravity on the moon is significantly lower than that on Earth. The moon has about one-sixth the gravity of Earth, which means objects weigh less on the moon compared to Earth. This lower gravity is due to the moon's smaller mass and smaller radius compared to Earth.

As a result, astronauts experience a different gravitational environment on the moon, which affects their movements and the energy required to perform tasks such as climbing.

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The resultant of two displacement vectors having opposite directions is the difference of the two displacements, having the same direction as the smaller vector.

When two displacement vectors have opposite directions, it means they are pointing in opposite ways. In other words, one vector is in the opposite direction of the other. To find the resultant of these vectors, we need to subtract one vector from the other.

If we consider two displacement vectors, let's say vector A and vector B, and they have opposite directions, we can represent them as A and -B.

To find the resultant, we subtract vector B from vector A: A - (-B) or A + B.

The resultant will have the same direction as the smaller vector. This is because when we subtract a larger vector from a smaller vector, the resultant will have the direction of the smaller vector.

Therefore, the correct option is: "The resultant is the difference of the two displacements, having the same direction as the smaller vector."

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The speed of the air during the motion of the helicopter is 188 km/h.

The speed of the helicopter, v₁ = 220 km/h

The speed of wind, v₂ = 32 km/h

The speed of one moving body in comparison to another is referred to as the relative speed.

The relative speed of two bodies travelling in the same direction is determined by the speed differential between them.

The expression for the relative speed is given by,

Relative speed = v₁ - v₂

Therefore, the speed of the air is given by,

v = v₁ - v₂

v = 220 - 32

v = 188 km/h

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The pressure of a tank of uniform cross-sectional area 4.0m2 when the tank is filled with water at a depth of 6m is 58800 Pa.

To find the pressure in the tank, we can use the formula for pressure:

Pressure = density x gravity x height

Density of water (ρ) = 1000 kg/m³

Acceleration due to gravity (g) = 9.8 m/s²

Height (h) = 6 m

Thus:

Pressure = 1000 kg/m³ x 9.8 m/s² x 6 m

Pressure = 58800 kg/(m·s²)

Since the unit of pressure is Pascal (Pa), which is equivalent to kg/(m·s²), the pressure in the tank is:

Pressure = 58800 Pa

Therefore, the pressure in the tank when it is filled with water to a depth of 6 m is 58800 Pascal.

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According to figure where the point P is located so that the magnitude of the Field at point p= Zero electric field will be [tex]E=\frac{1}{4\pi \epsilon_0s^3} \sqrt{q^2d^2}[/tex].

The electric field is a fundamental concept in physics that describes the force experienced by a charged particle in the presence of other charges. It is a vector field, which means it has both magnitude and direction at each point in space.

The electric field is created by electric charges. A positive charge creates an outward electric field, while a negative charge creates an inward electric field.

The strength or magnitude of the electric field at a given point depends on the magnitude of the charge creating the field and the distance from that point to the charge.

E due to the dipole formed by charges at extreme end,

[tex]E_x=k_p/d^3[/tex] in the x-direction

E due to the charge at center

[tex]E_y=k_q/d^3[/tex]

Net electric field is,

[tex]E=\frac{1}{4\pi \epsilon_0s^3} \sqrt{q^2d^2}[/tex]. as p = 0.

Thus, the answer is  [tex]E=\frac{1}{4\pi \epsilon_0s^3} \sqrt{q^2d^2}[/tex].

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Your question seems incomplete, the probable complete question is:

According to figure below where the point P is located so that the magnitude of the Field at point p= Zero ?

The maximum velocity of the freighter relative to the shore is 4 m/s.

To determine the maximum velocity of the freighter relative to the shore, we need to consider the velocities of the river and the freighter separately and then combine them. Since the freighter needs to travel against the flow of the water, we subtract the velocity of the river from the maximum speed of the freighter relative to the river.

Given that the river flows at 3 m/s relative to the shore, and the maximum speed of the freighter relative to the river is 7 m/s, we can subtract the river's velocity from the maximum speed of the freighter:

Max velocity of freighter relative to shore = Max velocity of freighter relative to river - Velocity of river

Max velocity of freighter relative to shore = 7 m/s - 3 m/s

Max velocity of freighter relative to shore = 4 m/s

This means that the freighter can travel upstream at a maximum speed of 4 meters per second relative to the stationary shore while overcoming the 3 m/s current flowing downstream in the Savannah River.

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Answer:

5A

Explanation:

The angular acceleration of the drill is 1512.5 rad/s².

Time taken for the drill, t = 0.36 s

Angular velocity of the drill, ω = 5200 rpm = 544.5 rad/s

The change in angular velocity that a spinning object experiences per unit of time is expressed quantitatively as angular acceleration, also known as its rotational acceleration.

It is a vector quantity that has two distinct directions or senses as well as a component of magnitude. The unit of angular acceleration is rad/s².

So,

The expression for the angular acceleration is given by,

α = ω/t

α = 544.5/0.36

α = 1512.5 rad/s²

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