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Use a circular pendulum to determine . You can increase the accuracy of the time it takes to go around once by timingN revolutions and then dividing by N. This minimizes errors contributed by inaccuracies in starting and stopping the clock. It is wise to start counting from zero (0,1,2,3,4,5)rather than starting from (0,1,2,3,4,5)represents only four revolutions, not five). It also improves accuracy if you start and stop timing at a well-defined event, such as when the mass crosses in front of an easily visible mark. This was the method used by Newton to get an accurate value of g. Newton was not only a brilliant theorist but also an excellent experimentalist. For a circular pendulum, he built a large triangular wooden frame mounted on a vertical shaft, and he pushed this around and around while making sure that the string of the circular pendulum stayed parallel to the slanting side of the triangle.

Short Answer

Expert verified

After ten repetitions of the same measurement, the value of g, which is close to the value of 9.8m/s2.

Step by step solution

01

The time of the pendulum

The pendulum's length is l=1m.

Determine how long it took the pendulum to complete 10 oscillationsN=10. You know that the pendulum's period is defined by the following formulas.

T=2πlg

Here, gis the acceleration due to gravity and lis the length.

And,

T=tN

Here,tis time and N is the number of oscillations.

According to 10 different time t,

t1=20.020s,t2=19.929s,t3=20.071s,t4=19.899s,t5=20.030s,t6=19.989s,t7=20.081s,t8=19.909s,t9=20.112s,t10=19.949s

02

The value of g

The formula must be inverted above to calculate g.

tN=2πlglg=t2πN/2lg=t24π2N2

g=4π2lN2t2 ….. (1)

The constant part of the formula is:

4π2lN2=4×3.142×1m×102=3943.84m

03

The average value of g

Use equation (1) for time t1as below.

g1=4π2lN2t12=3943.84m20.020s2=9.84m/s2

Use equation (1) for time t2as below.

g2=4π2lN2t22=3943.84m19.929s2=9.93m/s2

Use equation (1) for time t3as below.

g3=4π2lN2t32=3943.84m20.071 s2=9.79m/s2

Use equation (1) for time t4as below.

g4=4π2lN2t42=3943.84m19.899 s2=9.96m/s2

Use equation (1) for time t5as below.

g5=4π2lN2t52=3943.84m20.03 s2=9.83m/s2

Use equation (1) for time t6as below.

g6=4π2lN2t62=3943.84m19.989 s2=9.87m/s2

Use equation (1) for time t7as below.

g7=4π2lN2t72=3943.84m20.081 s2=9.78m/s2

Use equation (1) for time t8as below.

g8=4π2lN2t82=3943.84m19.909 s2=9.95m/s2

Use equation (1) for time t9as below.

g9=4π2lN2t92=3943.84m20.112 s2=9.75m/s2

Use equation (1) for time t10as below.

g10=4π2lN2t102=3943.84m19.949 s2=9.91m/s2

The average value of g is:

g=g1+g2+g3+g4+g5+g6+g7+g8+g9+g1010

Substitute the known values in the above equation.

g=9.84+9.93+9.79+9.96+9.83+9.87+9.78+9.95+9.75+9.91m/s210=98.61m/s210=9.86m/s2

After ten repetitions of the same measurement, the value of gwas achieved, which is close to the value of 9.86m/s2.

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Most popular questions from this chapter

(a) Many communication satellites are placed in a circular orbit around the Earth at a radius where the period (the time to go around the Earth once) is\(24\;{\rm{h}}\). If the satellite is above some point on the equator, it stays above that point as the Earth rotates, so that as viewed from the rotating Earth the satellite appears to be motionless. That is why you see dish antennas pointing at a fixed point in space. Calculate the radius of the orbit of such a "synchronous" satellite. Explain your calculation in detail.

(b) Electromagnetic radiation including light and radio waves travels at a speed of\(3 \times {10^8}\;{\rm{m}}/{\rm{s}}\). If a phone call is routed through a synchronous satellite to someone not very far from you on the ground, what is the minimum delay between saying something and getting a response? Explain. Include in your explanation a diagram of the situation.

(c) Some human-made satellites are placed in "near-Earth" orbit, just high enough to be above almost all of the atmosphere. Calculate how long it takes for such a satellite to go around the Earth once, and explain any approximations you make.

(d) Calculate the orbital speed for a near-Earth orbit, which must be provided by the launch rocket. (The advantages of near-Earth communications satellites include making the signal delay unnoticeable, but with the disadvantage of having to track the satellites actively and having to use many satellites to ensure that at least one is always visible over a particular region.)

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