How to approach a fluid dynamics problem

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shreddinglicks
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Homework Statement


Homework problem text: "1. Show that at θ = 66.8°, the wind speed on the cliff described by ψ = 0 in Fig. 4.1 is the same as that far upstream."


Contour plot of streamlines for a uniform flow plus source, with solid streamlines labelled by psi values and dashed lines of psi1 and psi2, and a stagnation point marked A and B' on the horizontal axis; caption reads Fig. 4.1.

Homework Equations


Equations for a stream function: psi = psi1 + psi2 = -V_inf y + (Lambda/2pi) theta, then = V_inf (h theta / pi - y).


The Attempt at a Solution


I don't even know where to start. I don't understand the question.
 
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Have you learned that the speed of the flow is proportional to the magnitude of the gradient of the stream function?
 
Chestermiller said:
Have you learned that the speed of the flow is proportional to the magnitude of the gradient of the stream function?
do you mean

V^2=u^2+v^2

where
Two equations of the Cauchy-Riemann type: u = partial phi over partial x = partial psi over partial y, and v = partial phi over partial y = negative partial psi over partial x.
 
Chestermiller said:
Yes. But you need to express theta in terms of x and y to evaluate these derivatives.(except, of course, far upstream).
So would it be better to use
Equations for stream function velocity components: u_r = (1/r) ∂ψ/∂θ; u_θ = −∂ψ/∂r.

and make y = rsin(theta)
 
Chestermiller said:
Yes. But you need to express theta in terms of x and y to evaluate these derivatives.(except, of course, far upstream).
Wait, I see what you mean
Handwritten equation: theta = tan^-1(y/x), with y over x as a fraction inside the inverse tangent.
 
Chestermiller said:
I'm not going to check your math. I leave it to you to get the math correct.
That's fine. I'm not here to learn math. Since I now have V^2 what do I do from here? I still don't understand the question I need to solve.
 
You need to show that, at the x and y corresponding to theta = 66.8 degrees and psi = 0, the speed is the same as at y = 0, x = infinity
 
Last edited:
Chestermiller said:
You need to show that, at the x and y corresponding to theta = 66.8 degrees and psi = 0, the speed is the same as at y = 0, x = - infinity
So I know at a large value of -x and y= o that my V^2 is equal to 1.

would it be appropriate to sub in
x=rcos(theta)
y=rsin(theta)
r=x^2+y^2
and then plug in 66.8 = theta
 
shreddinglicks said:
So I know at a large value of -x and y= o that my V^2 is equal to 1.

would it be appropriate to sub in
x=rcos(theta)
y=rsin(theta)
r=x^2+y^2
and then plug in 66.8 = theta
You have to evaluate it at psi = 0.
 
Chestermiller said:
You have to evaluate it at psi = 0.
Bernoulli eq?
 
Chestermiller said:
What about it?
The only thing I can think of that would relate the velocity eq and pressure would be that. Is that what I should be using?
 
shreddinglicks said:
The only thing I can think of that would relate the velocity eq and pressure would be that. Is that what I should be using?
No. You should be setting psi = 0 and theta = 66.8 degrees (in radians). This gives you an equation for y. Once you know y and theta, you know x.
 
Chestermiller said:
No. You should be setting psi = 0 and theta = 66.8 degrees (in radians). This gives you an equation for y. Once you know y and theta, you know x.
I see exactly what you mean. I must be losing my mind thinking psi is pressure. I did exactly what you said and got x and y. I plugged into the the V^2 equation and got 1 as my answer.
 
Thanks for helping me. I can sleep easy tonight. You are the man Chestermiller!