Nonsimilar Boundary-Layer Heat Transfer of a Rotating Cone in Forced Flow

[+] Author and Article Information
J. C. Y. Koh

Aerospace Division, The Boeing Company, Seattle, Wash.

J. F. Price

Scientific Research Laboratories, The Boeing Company, Seattle, Wash.

J. Heat Transfer 89(2), 139-145 (May 01, 1967) (7 pages) doi:10.1115/1.3614336 History: Received June 01, 1965; Revised April 25, 1966; Online August 25, 2011


The nonsimilar boundary-layer flow and heat transfer of a cone rotating in a forced-flow field are investigated. Numerical solutions are shown for a half-cone angle of 53.5 deg with parameters (vw /ue )2 ranging from 0 to 20, and with Prandtl numbers from 0.2 to 10. With a half-cone angle of 90 deg (so that one has a rotating disk), the degenerate problem is solved in the same manner.

Copyright © 1967 by ASME
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