. (Subsonic flight) The efficiency of the engines of subsonic airplanes depends on air pressure and usually is maximum near about 36 000 ft. Find the air pressure y(x) at this height without calculation. Physical information. The rate of change y'(x) is proportional to the pressure, and at 18 000 ft the pressure has decreased to half its value yo at sea level.

Calculus: Early Transcendentals
8th Edition
ISBN:9781285741550
Author:James Stewart
Publisher:James Stewart
Chapter1: Functions And Models
Section: Chapter Questions
Problem 1RCC: (a) What is a function? What are its domain and range? (b) What is the graph of a function? (c) How...
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. Calculation of change in pressure.
Find the air pressure at the height
using differential equation (disregard
the without calculation)
. (Subsonic flight) The efficiency of the engines of
subsonic airplanes depends on air pressure and usually
is maximum near about 36 000 ft. Find the air pressure
y(x) at this height without calculation. Physical
information. The rate of change y'(x) is proportional
to the pressure, and at 18 000 ft the pressure has
decreased to half its value yo at sea level.
Transcribed Image Text:. Calculation of change in pressure. Find the air pressure at the height using differential equation (disregard the without calculation) . (Subsonic flight) The efficiency of the engines of subsonic airplanes depends on air pressure and usually is maximum near about 36 000 ft. Find the air pressure y(x) at this height without calculation. Physical information. The rate of change y'(x) is proportional to the pressure, and at 18 000 ft the pressure has decreased to half its value yo at sea level.
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