SOLUTION: The altitude of an aircraft, h, in miles, is given by
h= - (100/9)log p/b
where P = the outside pressure and B = the atmospheric pressure at sea level. Let B = 31 inches of mer
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-> SOLUTION: The altitude of an aircraft, h, in miles, is given by
h= - (100/9)log p/b
where P = the outside pressure and B = the atmospheric pressure at sea level. Let B = 31 inches of mer
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Question 713101: The altitude of an aircraft, h, in miles, is given by
h= - (100/9)log p/b
where P = the outside pressure and B = the atmospheric pressure at sea level. Let B = 31 inches of mercury. What is the outside air pressure at a height of 2.7 miles? Round your answer to the nearest tenth.
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Substituting in the values given for b and h we get:
And now we solve for p. First we'll isolate the log. Multiplying both sides by -9/100:
Next we rewrite the equation in exponential form. In general is equivalent to . Using this pattern (and the fact that the base of "log" is 10) on our equation we get:
Next we multiply both sides by 31:
This is an exact expression for the solution. I'll leave it up to you to use your calculator to find the decimal. (Just be sure to raise 10 to the -.243 power before you multiply by 31.)