Accession Number:
AD0262482
Title:
EFFECTS OF UNIT REYNOLDS NUMBER, NOSE BLUNTNESS, AND ROUGHNESS ON BOUNDARY LAYER TRANSITION
Descriptive Note:
Corporate Author:
ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (FRANCE)
Personal Author(s):
Report Date:
1960-04-01
Pagination or Media Count:
84.0
Abstract:
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.
Descriptors:
Subject Categories:
- Fluid Mechanics