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Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation. Part 1: Summary reportThe analysis uses a compressibility transformation and utilizes higher order closure rules to complete the transformation. By requiring that the momentum equations in differential form be satisfied at the wall and at the sublayer edge, correspondence rules are obtained which relate the variable property (VP) flow to a constant property (CP) flow in which mass transfer and pressure gradient occur simultaneously. A new CP formulation is developed and numerical results for a variety of cases are presented. Comparisons with earlier forms of the transformation and with experiment are included. For the zero pressure gradient case some differences between the various predictions are observed. For the several pressure gradient cases examined, the results are found to be essentially identical to those given by first order closure rules; i.e., by a form of transformation which relates the VP flow to a CP flow with pressure gradient but zero mass transfer.
Document ID
19720004577
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Economos, C.
(General Applied Science Labs., Inc. Westbury, NY, United States)
Boccio, J.
(General Applied Science Labs., Inc. Westbury, NY, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1971
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics
Report/Patent Number
GASL-TR-748-PT-1
NASA-CR-1923
Accession Number
72N12226
Funding Number(s)
CONTRACT_GRANT: NAS1-9624
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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