Mixing length in low Reynolds number compressible turbulent boundary layers
Abstract
The paper studies the effect of low Reynolds number in high-speed turbulent boundary layers on variations of mixing length. Boundary layers downstream of natural transition on plates, cones and cylinders, and boundary layers on nozzle walls without laminarization-retransition are considered. The problem of whether low Reynolds number amplification of shear stress is a result of transitional flow structure is considered. It is concluded that a knowledge of low Reynolds number boundary layer transition may be relevant to the design of high-speed vehicles.
- Publication:
-
AIAA Journal
- Pub Date:
- August 1975
- DOI:
- 10.2514/3.60510
- Bibcode:
- 1975AIAAJ..13.1119B
- Keywords:
-
- Compressible Flow;
- Mixing Length Flow Theory;
- Reynolds Number;
- Turbulent Boundary Layer;
- Flow Distribution;
- Mach Number;
- Shear Stress;
- Wall Flow;
- Wall Temperature;
- Fluid Mechanics and Heat Transfer