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beks73 [17]
4 years ago
11

As computer structures get smaller and smaller, quantum rules start to create difficulties. Suppose electrons move through a cha

nnel in a microprocessor. If we know that an electron is somewhere along the 50 nm length of the channel, what is ∆vx? If we treat the elec- tron as a classical particle moving at a speed at the outer edge of the uncertainty range, how long would it take to traverse the channel?
Physics
1 answer:
nadezda [96]4 years ago
6 0

Answer:

a) ∆x∆v = 5.78*10^-5

   ∆v = 1157.08 m/s

b) 4.32*10^{-11}

Explanation:

To solve this problem you use the Heisenberg's uncertainty principle, that is given by:

\Delta x\Delta p \geq \frac{\hbar}{2}

where h is the Planck's constant (6.62*10^-34 J s).

If you assume that the mass of the electron is constant you have:

\Delta x \Delta (m_ev)=m_e\Delta x\Delta v \geq \frac{\hbar}{2}

you use the value of the mass of an electron (9.61*10^-31 kg), and the uncertainty in the position of the electron (50nm), in order to calculate ∆x∆v and ∆v:

\Delta x \Delta v\geq\frac{\hbar}{2m_e}=\frac{(1.055*10^{-34}Js)}{2(9.1*10^{-31}kg)}=5.78*10^{-5}\ m^2/s

\Delta v\geq\frac{5.78*10^{-5}}{50*10^{-9}m}=1157.08\frac{m}{s}

If the electron is a classical particle, the time it takes to traverse the channel is (by using the edge of the uncertainty in the velocity):

t=\frac{x}{v}=\frac{50*10^{-9}m}{1157.08m/s}=4.32*10^{-11}s

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Which equations could be used as is, or rearranged to calculate for frequency of a wave? Check all that apply.
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-- Equations  #2  and  #6  are both the same equation,
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-- If you divide each side by  'wavelength', you get Equation #4,
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-- If you divide each side by  'frequency', you get Equation #3,
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Summary:

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What is another name for the surface of the sun?
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6 0
3 years ago
A satellite orbits the earth a distance of 1.50 × 107 m above the planet's surface and takes 8.65 hours for each revolution abou
kupik [55]

Answer:

The acceleration of the satellite is 0.87 m/s^{2}

Explanation:

The acceleration in a circular motion is defined as:

a = \frac{v^{2}}{r}  (1)

Where a is the centripetal acceleration, v the velocity and r is the radius.

The equation of the orbital velocity is defined as

v = \frac{2 \pi r}{T} (2)

Where r is the radius and T is the period

For this particular case, the radius will be the sum of the high of the satellite (1.50x10^{7} m) and the Earth radius (6.38x10^{6} m) :

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Then, equation 2 can be used:

T = 8.65 hrs \cdot \frac{3600 s}{1hrs} ⇒ 31140 s

v = \frac{2 \pi (21.38x10^{6}m)}{31140s}

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