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

Similar Questions

Consider the differential equation with initial conditions y = 0 and dy/dx = 1 at x = 1. The value of y at x = 2 is _______. (round off to two decimal place...
#127 Fill in the Blanks
Consider the differential equation d2y/dx2 - 2(dy/dx) + y = 0. The boundary conditions are y = 0 and dy/dx = 1 at x = 0. Then the value of y at x = 1/2 is _____...
#175 MCQ
Consider the differential equation and the boundary conditions d2y/dx2 + 8(dy/dx) + 16y = 0, y(0) = 1 and dy/dx(0) = 0. The solution to this equation is: ______...
#214 MCQ

Related Topics

Aerospace Engineering GATE 2018 GATE AE 2018 Q27 steady isentropic flow pressure velocity relation compressible flow fluid mechanics aerospace Bernoulli's equation compressible isentropic flow equation

Unique Visitor Count

Total Unique Visitors

Loading......