According to the U.S. standard atmospheric model, developed by the National Oceanic and Atmospheric Administration for use

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According to the U.S. standard atmospheric model, developed by the National Oceanic and Atmospheric Administration for use in aircraft and rocket design, atmospheric temperature T (in degrees Celsius), pressure P (kPa = 1000 pascals), and altitude h (in meters) are related by these formulas (valid in the troposphere h ≤ 11,000):

T 15.040.00649h, = P = 101.29 T + 273.1 288.08 5.256

Use the Chain Rule to calculate dP/dh.

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Calculus

ISBN: 9781319055844

4th Edition

Authors: Jon Rogawski, Colin Adams, Robert Franzosa

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