EFFECTS OF UNIT REYNOLDS NUMBER, NOSE BLUNTNESS, AND ROUGHNESS ON BOUNDARY LAYER TRANSITION
ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (FRANCE)
Pagination or Media Count:
This analysis consists of two parts. A technique is presented for measuring heat transfer rates on a model and for fixing the temperature distribution at a given value. The technique is applied to the particular case of turbulent heat transfer on a blunt body at a Mach number of 3.98.
- Fluid Mechanics