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Plume characteristics of single-stream and dual-flow conventional and inverted-profile nozzles at equal thrustThe plume velocity and temperature decay rates of single-stream, conventional dual-flow and inverted-profile dual-flow nozzles are compared at equal values of ideal thrust over a wide range of flow conditions. The comparisons are made in terms of constant velocity and temperature contour maps. The results show that both dual-flow nozzle types have much greater plume velocity and temperature decay rates than those of equivalent thrust single-stream nozzles when the respective secondary flows were at ambient temperature. With hot secondary flows, the inverted-profile dual-flow plumes decayed significantly faster than those of single-stream nozzles; however, the decay rates for the conventional dual-flow streams were about the same as those for the single-stream nozzles. Consequently, with hot secondary flows, the inverted-profile dual-flow plumes decayed much faster than the conventional dual-flow plumes at equal thrust.
Document ID
19860016813
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vonglahn, U. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Goodykoontz, J. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:87323
AIAA PAPER 86-1809
NASA-TM-87323
E-3060
Report Number: NAS 1.15:87323
Report Number: AIAA PAPER 86-1809
Report Number: NASA-TM-87323
Report Number: E-3060
Meeting Information
Meeting: Applied Aerodynamics Conference
Location: San Diego, CA
Country: United States
Start Date: June 9, 1986
End Date: June 11, 1986
Sponsors: AIAA
Accession Number
86N26285
Funding Number(s)
PROJECT: RTOP 506-62-91
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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