
Accession Number : AD0618482
Title : NONSIMILAR BOUNDARY LAYER HEAT TRANSFER OF A ROTATING CONE IN FORCED FLOW.
Descriptive Note : Mathematical note,
Corporate Author : BOEING SCIENTIFIC RESEARCH LABS SEATTLE WASH
Personal Author(s) : Koh,J. C. Y. ; Price,J. F.
Report Date : APR 1965
Pagination or Media Count : 30
Abstract : The problem of fluid flow and heat transfer characteristics of a cone rotating in a forced flow field is investigated. The flow problem in general involves two parameters, m and s. For heat transfer, one additional parameter, Pr, must be considered. For the special case of a rotating disk in forced flow, the partial differential equations are reduced to a set of ordinary differential equations with two parameters s and Pr. The nonsimilar boundary layer flow equations are solved for two half cone angles (alpha = 90 degrees and 53.5 degrees) for various Prandtl numbers with s ranging from 0 to about 20. It was found that for s = 10, the first order approximation from the power expansion scheme may not be sufficient. (Author)
Descriptors : (*HEAT TRANSFER, BOUNDARY LAYER), (*CONICAL BODIES, HEAT TRANSFER), ROTATION, FLUID FLOW, HEAT TRANSFER COEFFICIENTS, PARTIAL DIFFERENTIAL EQUATIONS, DISKS, DRAG, TORQUE
Distribution Statement : APPROVED FOR PUBLIC RELEASE