Question Details

The steady velocity field in an inviscid fluid of density 1.5 is given to be  V = ( y 2 x 2 ) i ^ + ( 2 x y ) j ^ . Neglecting body forces, the pressure gradient at (x =1, y = 1) is ______.

Options

A

10 ĵ

B

20 î

C

-6î - 6ĵ

D

-4î - 4ĵ

Correct Answer :

-6î - 6ĵ

Solution :

The correct option is -6î - 6ĵ.

1. Understanding the Governing Equation
For a steady, inviscid flow neglecting body forces, the motion of the fluid is governed by Euler's equation of motion:


ρ a = - P

where:
ρ is the density of the fluid (given as 1.5),
a is the acceleration vector, and
P is the pressure gradient vector.
Rearranging the equation, we can write the pressure gradient as:


P = - ρ a

2. Determining the Velocity Components and Derivatives
The given velocity field is:


V = ( y 2 - x 2 ) i ^ + ( 2 x y ) j ^

From this, the horizontal velocity component u and vertical velocity component v are:


u = y 2 - x 2


v = 2 x y

Now, let's calculate the required partial derivatives of the velocity components with respect to x and y:


u x = - 2 x


u y = 2 y


v x = 2 y


v y = 2 x

3. Calculating Acceleration Components at (x = 1, y = 1)
First, evaluate the velocity components u and v at the point (1,1):


u = 1 2 - 1 2 = 0


v = 2 ( 1 ) ( 1 ) = 2

For steady flow, the local acceleration is zero, so the acceleration components are solely convective:


a x = u u x + v u y = ( 0 ) ( - 2 ) + ( 2 ) ( 2 ) = 4


a y = u v x + v v y = ( 0 ) ( 2 ) + ( 2 ) ( 2 ) = 4

Thus, the acceleration vector at the point (1,1) is:


a = 4 i ^ + 4 j ^

4. Computing the Pressure Gradient
Substitute the fluid density ρ=1.5 and the computed acceleration vector a back into Euler's relation:


P = - 1.5 ( 4 i ^ + 4 j ^ ) = - 6 i ^ - 6 j ^

Therefore, the pressure gradient at (x=1,y=1) is indeed -6î - 6ĵ.

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