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Pitot pressure measurements in flow fields behind circular-arc nozzles with exhaust jets at subsonic free-stream Mach numbersThe flow field behind a circular arc nozzle with exhaust jet was studied at subsonic free stream Mach numbers. A conical probe was used to measure the pitot pressure in the jet and free stream regions. Pressure data were recorded for two nozzle configurations at nozzle pressure ratios of 2.0, 2.9, and 5.0. At each set of test conditions, the probe was traversed from the jet center line into the free stream region at seven data acquisition stations. The survey began at the nozzle exit and extended downstream at intervals. The pitot pressure data may be applied to the evaluation of computational flow field models, as illustrated by a comparison of the flow field data with results of inviscid jet plume theory.
Document ID
19800003816
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mason, M. L.
(NASA Langley Research Center Hampton, VA, United States)
Putnam, L. E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
L-13060
NASA-TM-80169
Report Number: L-13060
Report Number: NASA-TM-80169
Accession Number
80N12066
Funding Number(s)
PROJECT: RTOP 505-32-13-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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