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Analytical skin friction and heat transfer formula for compressible internal flowsAn analytic, closed-form friction formula for turbulent, internal, compressible, fully developed flow was derived by extending the incompressible law-of-the-wall relation to compressible cases. The model is capable of analyzing heat transfer as a function of constant surface temperatures and surface roughness as well as analyzing adiabatic conditions. The formula reduces to Prandtl's law of friction for adiabatic, smooth, axisymmetric flow. In addition, the formula reduces to the Colebrook equation for incompressible, adiabatic, axisymmetric flow with various roughnesses. Comparisons with available experiments show that the model averages roughly 12.5 percent error for adiabatic flow and 18.5 percent error for flow involving heat transfer.
Document ID
19940020691
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dechant, Lawrence J.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Tattar, Marc J.
(Ohio Aerospace Inst. Brook Park., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-191185
NAS 1.26:191185
E-8096
Accession Number
94N25173
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
PROJECT: RTOP 505-69-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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