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The Effect of Cooling Passage Aspect Ratio on Curvature Heat Transfer EnhancementA series of electrically heated tube experiments was performed to investigate the effect of high aspect ratio on curvature heat transfer enhancement in uniformly heated rectangular cooling passages. Three hardware geometries were tested: a baseline straight aspect ratio 10 tube, an aspect ratio 1 (square) tube with a 45 deg. curve, and an aspect ratio 10 tube with a 45 deg. curve. Gaseous nitrogen with the following properties was used as the coolant: ambient inlet temperature, pressures to 8.3 MPa, wall-to-bulk temperature ratios less than two, and Reynolds numbers based on hydraulic diameter ranging from 250,000 to 1,600,000. The measured curvature enhancement factors were compared to values predicted by three previously published models which had been developed for low aspect ratio tubes. The models were shown to be valid for the high aspect ratio tube as well the low aspect ratio tube, indicating that aspect ratio had little impact on the curvature heat transfer enhancement in these tests.
Document ID
19970012643
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Meyer, Michael L.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1997
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
E-10672
NASA-TM-107426
NAS 1.15:107426
Report Number: E-10672
Report Number: NASA-TM-107426
Report Number: NAS 1.15:107426
Accession Number
97N16895
Funding Number(s)
PROJECT: RTOP 505-62-7K-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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