Abstract
The Prandtl's layer equations was considered for laminar flow past a plate with suction/blowing of the flow rate density v0(x) = ∓v i2∓1/2RE1/2x ∓1/2. It was found that Reynolds number was large the solution of the problem had a parabolic boundary layer at the surface of the plate excluding its leading edge. A direct numerical method for computing approximations to the solution of this problem using a piecewise uniform fitted mesh technique was also constructed. It was also shown by extensiv.
Original language | English |
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Pages (from-to) | 387-402 |
Number of pages | 16 |
Journal | International Journal of Computational Engineering Science |
Volume | 5 |
Issue number | 2 |
DOIs | |
Publication status | Published - Jun 2004 |
Keywords
- Boundary layer equations
- Finite difference
- Prandtl's problem with mass transfer
- Reynolds uniform direct numerical method