Aerodynamics HW - fluid particles acceleration based on stream functio

AI Thread Summary
The discussion revolves around proving the acceleration of fluid particles in a corner flow described by the stream function ψ=Axy. The user calculates the velocity components as U=Ax and V=-Ay, leading to an expression for acceleration. However, confusion arises regarding the origin of the term involving r and the expression (x²-y²). A suggestion is made to first determine the vector components of acceleration before calculating its magnitude, emphasizing that the user’s current approach does not yield the expected results. The conversation highlights the importance of correctly applying fluid dynamics equations to derive accurate results.
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Homework Statement


prove that with flow in a corner, with stream function ψ=Axy, particles are accelerating per \frac{DV}{Dt}=(A2(x2-y2))/r; A=const; r-distance from the center of the corner


Homework Equations



Vx=U=\frac{∂ψ}{∂y} . . Vy=V=-\frac{∂ψ}{∂x}

a=\frac{∂V}{∂t}+U\frac{∂V}{∂x}+\frac{∂V}{∂y}

The Attempt at a Solution



As per above equations i get velocity components as
U=Ax and V=-Ay


then since local acc is 0 acceleration is:

a=Ax\frac{A(x-y)}{∂x} - Ay\frac{A(x-y)}{∂y}

finally, as per my calcs, accelerations is:

a=A2(x+y)

where did this r come from and also (x2-y2). i was thinking using r2=x2+y2, and using to multiply the whole acceleration expression with r2/(x2+y2), but i am getting nowhere.

help please
 
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Your equation does not give the acceleration. The acceleration is a vector, and you need to find its components first, before determining its magnitude.

a_x=u\frac{∂u}{∂x}+v\frac{∂u}{∂y}
a_y=u\frac{∂v}{∂x}+v\frac{∂v}{∂y}

Even with this, you still don't match the answer you are trying to prove.

Chet
 
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