Circular Motion Problems: Solving for Speed, Period, and Acceleration

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SUMMARY

This discussion focuses on solving circular motion problems related to speed, period, and acceleration. Key calculations include determining the speed a plane must fly along the Earth's equator to keep the sun stationary relative to passengers, which requires understanding the Earth's rotation and radius of 6400 km. Additionally, it addresses the period of a geosynchronous satellite orbiting at an altitude of 3.58 x 107 m and the gravitational acceleration at that altitude. Lastly, it explores the dynamics of a 2.0 kg ball swinging in a vertical circle, including tension, speed, and acceleration at a specific angle.

PREREQUISITES
  • Understanding of circular motion principles
  • Knowledge of gravitational force calculations
  • Familiarity with the concept of geosynchronous orbits
  • Basic physics of tension in circular motion
NEXT STEPS
  • Calculate the speed of a plane flying along the equator using the formula for circular motion.
  • Learn how to derive the period of a satellite in a geosynchronous orbit using Kepler's laws.
  • Explore gravitational acceleration variations with altitude using the formula g = G*M/(r+h)2.
  • Analyze the forces acting on an object in circular motion to determine speed and acceleration at various angles.
USEFUL FOR

Students studying physics, educators teaching circular motion concepts, and anyone interested in understanding the dynamics of motion in gravitational fields.

ysk1
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I'm stuck on the questions below.
Please tell me how to solve them.
Thank you.


1. How fast must a plane fly along the Earth's equator so that the sun stands still relative to the passengers? In which direction must the plane fly, east to west or west to east? Give your answer in km/hr. The radius of the Earth is 6400 km.

2. Satellites are placed in a circular orbit where they stay directly over a fixed point on the equator as the Earth rotates. The altitude of a satellite's orbit is 3.58 x 10^7 m.
a. What is the priod of a satellite in a geosynchronous orbit?
b. Find the value of g at this altitude.

3. A 2.0 kg ball swings in a vertical circle on the end of an 80-cm-long string. The tension in the string is 20 N when its angle from the highest point on the circle is theta = 30 degrees.
a. What is the ball's speed when theta = 30 degrees?
b. What are the magnitude and direction of the ball's acceleration when theta = 30 degrees?
 
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ysk1 said:
I'm stuck on the questions below.
Please tell me how to solve them.
Thank you.


1. How fast must a plane fly along the Earth's equator so that the sun stands still relative to the passengers? In which direction must the plane fly, east to west or west to east? Give your answer in km/hr. The radius of the Earth is 6400 km.

2. Satellites are placed in a circular orbit where they stay directly over a fixed point on the equator as the Earth rotates. The altitude of a satellite's orbit is 3.58 x 10^7 m.
a. What is the priod of a satellite in a geosynchronous orbit?
b. Find the value of g at this altitude.

3. A 2.0 kg ball swings in a vertical circle on the end of an 80-cm-long string. The tension in the string is 20 N when its angle from the highest point on the circle is theta = 30 degrees.
a. What is the ball's speed when theta = 30 degrees?
b. What are the magnitude and direction of the ball's acceleration when theta = 30 degrees?
Please show us what you have tried to solve these problems
 
At least try to solve a portion of the problem. This could be ... I know the Earth spins at 1 revolution per day = 2 pi radians per day, and I know that the Earth is 3950 miles in radius. What do I do now?

At least put forth some question YOU have, not just post a question.
 

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