Answer:
A. 1236.49 lb/ft²
B. 1037.21 lb/ft²
C 2269.7 lb/ft²
Explanation:
P = pa(1-βz/Ta)^g/Rβ
a.)
Pa [1-(0.00357)(14110)/518.67]^32.2/1716*0.00357
= 2116.2(1-0.09712)^5.26
= 2116.2(0.5843)
= 1236.49566 lb/ft²
b.)
Pressure at higher elevation
P = Pa - yz
= 2116.2-(0.07647)(14110)
= 1037.2083 lb/ft³
C.
Pressure at higher elevation if air is isothermal
= (Pa)*exp[-(32.2)(14110)/(1716)(519)]
= 2116.2*exp[-454342/890604]
= 1269.7 lb/ft²