Engineering prediction of turbulent skin friction and heat transfer in high-speed flow

Author:: Bertram, M. H.
Published:: Jul 1, 1974.
Physical Description:: 1 electronic document
Additional Creators:: Cary, A. M., Jr.

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Summary:

A large collection of experimental turbulent-skin-friction and heat-transfer data for flat plates and cones was used to determine the most accurate of six of the most popular engineering-prediction methods; the data represent a Mach number range from 4 to 13 and ratio of wall to total temperature ranging from 0.1 to 0.7. The Spalding and Chi method incorporating virtual-origin concepts was found to be the best prediction method for Mach numbers less than 10; the limited experimental data for Mach numbers greater than 10 were not well predicted by any of the engineering methods except the Coles method.

Other Subject(s):

FLUID MECHANICS

Collection:

NASA Technical Reports Server (NTRS) Collection.

Note:

Document ID: 19740020652.
Accession ID: 74N28765.
L-9206.
NASA-TN-D-7507.

Terms of Use and Reproduction:

No Copyright.

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