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Boundary layer loss sensitivity study using a modified ICRPG turbulent boundary layer computer programModifications of the turbulent boundary layer (TBL) computer program refer to a more accurate representation of boundary layer edge conditions, internal calculation of the Prandtl number, a changed friction coefficient relationship, and computation of the performance degradation. Important input parameters of the modified TBL program such as wall temperature distribution, Prandtl number, Stanton number, and velocity profile exponent were changed and the individual effects on significant boundary layer parameters, heat transfer, and performance degradation are described.
Document ID
19720018582
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Omori, S.
(NAS-NRC Washington, D. C., United States)
Krebsbach, A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Gross, K. W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
March 3, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TM-X-64661
Report Number: NASA-TM-X-64661
Accession Number
72N26232
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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