Boundary layer thickness, accelerating flow.

Click For Summary
SUMMARY

The discussion focuses on the Falkner-Skan Wedge flow, which addresses boundary layer thickness over a flat plate with an increasing free stream velocity. The classic Blasius solution is not applicable in this scenario. The Falkner-Skan equation, represented as f''' + ff'' + β(1-f'^2) = 0, incorporates the power-law parameter β, which is derived from the free stream velocity distribution U(x) = Kx^m. This equation allows for the analysis of boundary layers under varying pressure gradients.

PREREQUISITES
  • Understanding of boundary layer theory
  • Familiarity with the Blasius solution
  • Knowledge of similarity solutions in fluid mechanics
  • Basic grasp of differential equations
NEXT STEPS
  • Study the Falkner-Skan equation and its applications in fluid dynamics
  • Research power-law velocity profiles and their implications on boundary layers
  • Explore dimensional analysis techniques for fluid mechanics problems
  • Review tables of solutions for the Falkner-Skan equation available in fluid mechanics literature
USEFUL FOR

Fluid mechanics students, researchers in aerodynamics, and engineers dealing with boundary layer analysis in accelerating flow scenarios will benefit from this discussion.

apc3161
Messages
20
Reaction score
0
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
 
Last edited by a moderator:
Engineering news on Phys.org
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.
 

Similar threads

  • · Replies 1 ·
Replies
1
Views
3K
  • · Replies 7 ·
Replies
7
Views
10K
  • · Replies 9 ·
Replies
9
Views
12K
  • · Replies 4 ·
Replies
4
Views
5K
Replies
4
Views
3K
Replies
1
Views
2K
  • · Replies 5 ·
Replies
5
Views
4K
  • · Replies 1 ·
Replies
1
Views
3K
  • · Replies 5 ·
Replies
5
Views
5K
  • · Replies 7 ·
Replies
7
Views
2K