Duplicate Question
The question on this page has been marked as a duplicate question.
Original Question
A ball falls from a tall bridge. The ball has a mass of 0.15 kg. The air density is 1.225 kg/m3 . The ball’s surface area is 0....Asked by hudson
Question
A ball falls from a tall bridge. The ball has a mass of 0.15 kg. The air density is 1.225 kg/m3
. The ball’s surface area is 0.0026 m2
. The ball’s coefficient of drag is 0.007. What is the ball’s terminal velocity?(1 point)
Responses
30.4 m/s
30.4 m/s
164 m/s
164 m/s
363 m/s
363 m/s
402 m/s
A ball falls from a tall bridge. The ball has a mass of 0.15 kg. The air density is 1.225 kg/m3
. The ball’s surface area is 0.0026 m2
. The ball’s coefficient of drag is 0.007. What is the ball’s terminal velocity?(1 point)
Responses
30.4 m/s
30.4 m/s
164 m/s
164 m/s
363 m/s
363 m/s
402 m/s
Answers
There are no human answers yet.
Answered by
GPT-4o mini
To find the terminal velocity of a falling ball, we can use the following formula for terminal velocity \(v_t\):
\[
v_t = \sqrt{\frac{2mg}{\rho C_d A}}
\]
where:
- \(m\) = mass of the object (kg)
- \(g\) = acceleration due to gravity (\(9.81 \, m/s^2\))
- \(\rho\) = air density (\(kg/m^3\))
- \(C_d\) = coefficient of drag
- \(A\) = surface area of the object (\(m^2\))
Now, substituting the values provided:
- \(m = 0.15 \, kg\)
- \(g = 9.81 \, m/s^2\)
- \(\rho = 1.225 \, kg/m^3\)
- \(C_d = 0.007\)
- \(A = 0.0026 \, m^2\)
Plugging in the values:
\[
v_t = \sqrt{\frac{2 \times 0.15 \times 9.81}{1.225 \times 0.007 \times 0.0026}}
\]
Calculating the numerator:
\[
2 \times 0.15 \times 9.81 = 2.943
\]
Calculating the denominator:
\[
1.225 \times 0.007 \times 0.0026 \approx 0.000022573
\]
Now calculating \(v_t\):
\[
v_t = \sqrt{\frac{2.943}{0.000022573}} \approx \sqrt{130175.8678} \approx 360.5 \, m/s
\]
Rounding gives us approximately \(363 \, m/s\).
Thus, the terminal velocity is \(\boxed{363 \, m/s}\).
\[
v_t = \sqrt{\frac{2mg}{\rho C_d A}}
\]
where:
- \(m\) = mass of the object (kg)
- \(g\) = acceleration due to gravity (\(9.81 \, m/s^2\))
- \(\rho\) = air density (\(kg/m^3\))
- \(C_d\) = coefficient of drag
- \(A\) = surface area of the object (\(m^2\))
Now, substituting the values provided:
- \(m = 0.15 \, kg\)
- \(g = 9.81 \, m/s^2\)
- \(\rho = 1.225 \, kg/m^3\)
- \(C_d = 0.007\)
- \(A = 0.0026 \, m^2\)
Plugging in the values:
\[
v_t = \sqrt{\frac{2 \times 0.15 \times 9.81}{1.225 \times 0.007 \times 0.0026}}
\]
Calculating the numerator:
\[
2 \times 0.15 \times 9.81 = 2.943
\]
Calculating the denominator:
\[
1.225 \times 0.007 \times 0.0026 \approx 0.000022573
\]
Now calculating \(v_t\):
\[
v_t = \sqrt{\frac{2.943}{0.000022573}} \approx \sqrt{130175.8678} \approx 360.5 \, m/s
\]
Rounding gives us approximately \(363 \, m/s\).
Thus, the terminal velocity is \(\boxed{363 \, m/s}\).
Submit Your Answer
We prioritize human answers over AI answers.
If you are human, and you can answer this question, please submit your answer.