Accession Number:
AD0609989
Title:
A TURBULENT BOUNDARY-LAYER CALCULATION METHOD BASED ON THE LAW OF THE WALL AND THE LAW OF THE WAKE
Descriptive Note:
Corporate Author:
NAVAL ORDNANCE TEST STATION CHINA LAKE CA
Personal Author(s):
Report Date:
1964-11-01
Pagination or Media Count:
79.0
Abstract:
The report presents the theoretical development of a method for calculating the incompressible turbulent boundary layer based on the law of the wall and the law of the wake. This development was carried out to provide a more rigorous solution of the boundary-layer equations for turbulent flow, in order to obtain an improved technique for estimating the inflow velocity profiles to propellers and the skin-friction drag of bodies of revolution.
Descriptors:
Subject Categories:
- Fluid Mechanics