Boundary layer thickness, accelerating flow.

AI Thread Summary
The discussion focuses on the challenge of determining boundary layer thickness over a flat plate with an increasing free stream velocity, which deviates from the classic Blasius solution that assumes constant velocity. A participant suggests that this scenario aligns with Falkner-Skan Wedge flow, which utilizes a similarity solution based on a power-law velocity distribution. The Falkner-Skan equation is introduced, highlighting its dependence on the power-law parameter and pressure gradient effects. Boundary conditions for this equation remain consistent with those for the flat plate scenario. Participants are encouraged to seek online resources for dimensionalizing the non-dimensional solutions relevant to their specific problems.
apc3161
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Hello,

You've all probably seen the classic Blasius solution concerning the thickness of a boundary over a flat plate. This problem though assumes that the free stream velocity is constant.

http://www.see.ed.ac.uk/~johnc/teaching/fluidmechanics4/2003-04/fluids9/2-dboundary.html

I am currently faced with a problem where the free stream velocity is increasing as you go down the plate, so I cannot use the Blasius solutions.

I was wondering if anyone out there knows anything about this subject and if they could reference me to some material concerning this topic.

Thanks
 
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It sounds to me like you have a Falkner-Skan Wedge flow. Basically this is a similarity solution (as the flat plate boundary layer). Similarity is achieved by the variable \eta = Cyx^a, which is consistent with a power-law freestream velocity distrubtion:
U(x) = Kx^m\,\,\,; m=2a+1
The exponent m may be termed the power-law parameter. do some blah blah blah, and the common form of the Falkner-Skan equation for similar flows is:
f''' + ff'' + \beta(1-f'^2) = 0
Where
\beta = \frac{2m}{1+m}
The boundary conditions are the same for the flat plate:
f(0) = f'(0) = 0; f'(\infty) = 1
Where the parameter \beta is a measure of the pressure gradient, and is positive for positive for a negative or favorable pressure gradient, and negative for an unfavorable pressure gradient; 0 denotes the flat plate.

I won't type the table out, but you should be able to find a table of solutions online somewhere. Basically they are all non-dimensional, so you'll have to find a reference to dimensionalize them to a real-life problem.
 
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