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Coolant pressure and airflow distribution in a strut-supported transpiration-cooled vane for a gas turbine engineAn analysis to predict pressure and flow distribution in a strut-supported wire-cloth vane was developed. Results were compared with experimental data obtained from room-temperature airflow tests conducted over a range of vane inlet airflow rates from 10.7 to 40.4 g/sec (0.0235 to 0.0890 lb/sec). The analytical method yielded reasonably accurate predictions of vane coolant flow rate and pressure distribution.
Document ID
19720021353
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Kaufman, A.
(NASA Lewis Research Center Cleveland, OH, United States)
Poferl, D. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Richards, H. T.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1972
Subject Category
Aircraft
Report/Patent Number
E-6800
NASA-TN-D-6916
Report Number: E-6800
Report Number: NASA-TN-D-6916
Accession Number
72N29003
Funding Number(s)
PROJECT: RTOP 764-74
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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