Chapter 3 Conceptual Project:

Under Pressure

The following table shows the atmospheric pressure p at the altitude of k feet above sea level (pressure is measured in mm Hg; note that this unit of pressure is approximately the pressure generated by a column of mercury 1 millimeter high).

k ( ft ) 0 1000 2000 3000 4000 5000 6000 7000 8000 9000 10,000
p ( mm Hg ) 760 733 707 681 656 632 609 586 564 543 523
  1. Find the average rate of change of air pressure from sea level to 2000 feet of altitude.

  2. Find the average rate of change of air pressure between the altitudes of 4000 and 10,000 feet.

  3. Use a symmetric difference quotient

    p c + h p c h 2 h

    to estimate the instantaneous rate of change of air pressure at 7000 ft by choosing h = 1000 ft .

  4. Tell whether you expect the answer to Question 2 or 3 to better approximate the instantaneous rate of change of air pressure at altitude 7000 ft . Explain. (Hint: Plotting the data on paper may help.)

  5. * Explain why you expect the symmetric difference quotient f c + h f c h 2 h in general to be a better approximation of the instantaneous rate of change of f at x = c than the "regular" difference quotient f c + h f c h .

  6. Use a graphing utility to find an exponential regression curve to the given data and plot the curve along with the data on the same screen.

  7. Use the exponential function you found in Question 6 to estimate the instantaneous rate of change of air pressure at 7000 ft , and compare with your estimate given in Question 3.

  8. Is the instantaneous rate of change increasing or decreasing with altitude? Explain.