Boundary-layer flow past a cylinder with massive blowing
Abstract
The effect of massive blowing on the unsteady laminar compressible boundary layer flow along the stagnation line of an infinite swept cylinder, when the freestream velocity and blowing rate vary with time, is studied. An implicit finite-difference scheme is used, together with the quasilinearization technique, to numerically solve the governing partial differential equations. Blowing is found to strongly affect skin friction, heat transfer, velocity, and total enthalpy profiles.
- Publication:
-
AIAA Journal
- Pub Date:
- November 1986
- DOI:
- 10.2514/3.9540
- Bibcode:
- 1986AIAAJ..24.1874N
- Keywords:
-
- Blowing;
- Boundary Layer Flow;
- Enthalpy;
- Stagnation Point;
- Unsteady Flow;
- Compressible Flow;
- Convective Heat Transfer;
- Cylindrical Bodies;
- Finite Difference Theory;
- Partial Differential Equations;
- Thermal Boundary Layer;
- Fluid Mechanics and Heat Transfer