Aerospace Engineering > GATE 2018 > Differential Equations
The relation between pressure (p) and velocity (V) for a steady, isentropic flow at two points along a streamline is, (c is a constant)
A
c(p2γ−p1γ)=V12/2−V22/2
B
c(p2γ/(γ−1)−p1γ/(γ−1))=V12/2−V22/2
C
c(p2(γ−1)/γ−p1(γ−1)/γ)=V12/2−V22/2
D
c(p2γ−1−p1γ−1)=V12/2−V22/2

Correct : c

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