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Designing A Transonic Nozzle For Efficient CoolingDesign for high-pressure transonic-flow nozzle increases effectiveness of coolant flowing in passages in wall nozzle. Revised curvatures of nozzle wall provide shortened transonic region and enable selection of approach- and discharge-wall angles for maximum cooling. Design enables wall to operate at lower temperature, reducing thermal fatigue and increasing life expectancy of wall. Also enables coolant to flow through wall channels with lower pressure drop and lower pumping pressure.
Document ID
19880000062
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Wagner, William R.
(Rockwell International Corp.)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Publication Information
Publication: NASA Tech Briefs
Volume: 12
Issue: 1
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
MFS-29224
Report Number: MFS-29224
ISSN: 0145-319X
Accession Number
88B10062
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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