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ddd [48]
3 years ago
13

The value of the gravitational acceleration g decreases with elevation from 9.807 m/s2 at the sea level to 9.767 m/s2 at an alti

tude of 13000 m, where large passenger planes cruise. Determine the percentage reduction in the weight of an airplane cruising at 13000 m relative to its weight at sea level.
Physics
1 answer:
alexira [117]3 years ago
6 0

Answer: 0.41%

Explanation:

If we want to calculate the percentage decrease (the reduction) in weight of an airplane, we can use the given values of gravity, because the weight is directly proportional to the gravity acceleration.

Now the formula for the percentage decrease for ths case is:

\% weightdecrease=\frac{g_{sea}-g_{13000m}}{g_{sea}}(100)

Where:

g_{sea}=9.807 m/s^{2} is the gravity at sea level

g_{13000m}=9.767 m/s^{2} is the gravity at 13000 m

\% weightdecrease=\frac{9.807 m/s^{2} - 9.767 m/s^{2}}{9.807 m/s^{2}}(100)

\% weightdecrease=0.00407 (100)

\% weightdecrease=0.407 \% \approx 0.41 \% This is the percentage reduction in the weight of an airplane

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Answer:

1.1\cdot 10^{-10}C

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Answer:

<em>A) the moment of inertia of the system decreases and the angular speed increases. </em>

Explanation:

The complete question is

A merry-go-round spins freely when Diego moves quickly to the center along a radius of the  merry-go-round. As he does this, It is true to say that

A) the moment of inertia of the system decreases and the angular speed increases.

B) the moment of inertia of the system decreases and the angular speed decreases.

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E) the moment of inertia of the system increases and the angular speed decreases

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and w_{1} and w_{2} are the initial and final angular speed respectively.

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