DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click
HERE to register or log in.
Accession Number:
AD0265910
Title:
The Thermal Laminar Boundary Layer On A Rotating Sphere.
Descriptive Note:
Corporate Author:
ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (FRANCE)
Report Date:
1960-04-01
Pagination or Media Count:
1.0
Abstract:
A method is developed for determining the thermal boundary layer of a rotating sphere in an incompressible fluid having uniform flow. The method follows an idea due to N. Frossling, in which the temperature distribution is expressed as a power series expansion. Use is made of results previously obtained by N. E. Hoskin for the velocity distribution in the laminar boundary layer of a rotating sphere. Numerical results, obtained with an IBM 704 computer, are included. Author
Distribution Statement:
APPROVED FOR PUBLIC RELEASE