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The speed of a transverse wave on a stretched string is given by the formula v = sqrt((T)/(mu)), where T is the tension in the string and mu is the linear mass density (mass per unit leng

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Part 17.1

The speed of a transverse wave on a stretched string is given by the formula v=Tμv = \sqrt{\frac{T}{\mu}}, where TT is the tension in the string and μ\mu is the linear mass density (mass per unit length) of the string. Both tension and linear density are properties of the medium that influence the speed of the wave. Wavelength and frequency are related to the speed (v=fλv = f\lambda) but do not determine the speed itself; rather, they are determined by the speed and each other.

Therefore, both Tension (A) and Linear density of the string (D) are factors that influence the speed of the wave. Since this is a multiple-choice question and typically only one answer is expected, we will select the first correct option listed.

The correct option is A.
A. Tension\boxed{\text{A. Tension}}

Part 17.2· 5 steps

The sound intensity level β\beta in decibels is related to the sound intensity II by the formula:

β=10log⁡10(II0)\beta = 10 \log_{10}\left(\frac{I}{I_0}\right)

where I0I_0 is the reference intensity, which is the threshold of human hearing, I0=1.0×10−12 W/m2I_0 = 1.0 \times 10^{-12}\,W/m^2.

  1. Set the given intensity level to 0 dB.

    0 dB=10log⁡10(II0)0\,dB = 10 \log_{10}\left(\frac{I}{I_0}\right)
  2. Divide by 10.

    0=log⁡10(II0)0 = \log_{10}\left(\frac{I}{I_0}\right)
  3. Convert the logarithmic equation to an exponential equation.

    100=II010^0 = \frac{I}{I_0} 1=II01 = \frac{I}{I_0}
  4. Solve for II.

    I=I0I = I_0
  5. Substitute the value of I0I_0.

    I=1.0×10−12 W/m2I = 1.0 \times 10^{-12}\,W/m^2

    The correct option is C.
    C. 1.0×10−12 W/m2\boxed{\text{C. } 1.0 \times 10^{-12}\,W/m^2}

Part 17.3· 5 steps

The speed of sound in an ideal gas is given by the formula:

v=γRTMv = \sqrt{\frac{\gamma RT}{M}}

where γ\gamma is the adiabatic index, RR is the ideal gas constant, TT is the absolute temperature, and MM is the molar mass of the gas.
From this formula, we can see that the speed of sound vv is directly proportional to the square root of the absolute temperature TT:

v∝Tv \propto \sqrt{T}
  1. Let the initial velocity be v1v_1 at an absolute temperature T1T_1.

    v1=kT1v_1 = k\sqrt{T_1}

    where k=γRMk = \sqrt{\frac{\gamma R}{M}} is a constant.

  2. If the absolute temperature is doubled, the new temperature T2=2T1T_2 = 2T_1.

  3. Calculate the new velocity v2v_2.

    v2=kT2=k2T1=2kT1v_2 = k\sqrt{T_2} = k\sqrt{2T_1} = \sqrt{2} k\sqrt{T_1}
  4. Substitute v1=kT1v_1 = k\sqrt{T_1} into the equation for v2v_2.

    v2=2v1v_2 = \sqrt{2} v_1
  5. Approximate the value of 2\sqrt{2}.

    2≈1.414\sqrt{2} \approx 1.414

    So, v2≈1.414v1v_2 \approx 1.414 v_1.

    The velocity of sound increases to approximately 1.4 times its original value.
    The correct option is A.
    A. It increases to 1.4 times its original value\boxed{\text{A. It increases to 1.4 times its original value}}

Part 17.4· 4 steps

This problem involves the Doppler effect for sound. When an observer approaches a stationary source, the observed frequency f′f' is given by the formula:

f′=f(v+vov)f' = f \left(\frac{v + v_o}{v}\right)

where ff is the source frequency, vv is the speed of sound in the medium, and vov_o is the speed of the observer.

  1. Identify the given values.

    Source frequency f=444 Hzf = 444\,Hz.
    Observer speed vo=12vv_o = \frac{1}{2}v (one-half the speed of sound).

  2. Substitute the values into the Doppler effect formula.

    f′=444 Hz(v+12vv)f' = 444\,Hz \left(\frac{v + \frac{1}{2}v}{v}\right)
  3. Simplify the expression inside the parentheses.

    f′=444 Hz(2v2+v2v)f' = 444\,Hz \left(\frac{\frac{2v}{2} + \frac{v}{2}}{v}\right) f′=444 Hz(3v2v)f' = 444\,Hz \left(\frac{\frac{3v}{2}}{v}\right) f′=444 Hz(32)f' = 444\,Hz \left(\frac{3}{2}\right)
  4. Calculate the observed frequency.

    f′=444 Hz×1.5f' = 444\,Hz \times 1.5 f′=666 Hzf' = 666\,Hz

    The correct option is A.
    A. 666 Hz\boxed{\text{A. } 666\,Hz}

Part 17.5

For a standing sound wave in a tube:

  • At a closed end, the air molecules cannot move, so there is no displacement. This point is a displacement node.
  • At an open end, the air molecules are free to move with maximum amplitude. This point is a displacement antinode.

Therefore, a standing sound wave in a tube opened at one end has a displacement node at the closed end and a displacement antinode at the open end.

The correct option is B.
B. node, antinode\boxed{\text{B. node, antinode}}

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