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Dispersion of turbojet engine exhaust in flightThe dispersion of the exhaust of turbojet engines into the atmosphere is estimated by using a model developed for the mixing of a round jet with a parallel flow. The analysis is appropriate for determining the spread and dilution of the jet exhaust from the engine exit until it is entrained in the aircraft trailing vortices. Chemical reactions are not expected to be important and are not included in the flow model. Calculations of the dispersion of the exhaust plumes of three aircraft turbojet engines with and without afterburning at typical flight conditions are presented. Calculated average concentrations for the exhaust plume from a single engine jet fighter are shown to be in good agreement with measurements made in the aircraft wake during flight.
Document ID
19730019442
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Holdeman, J. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1973
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-7382
E-7479
Report Number: NASA-TN-D-7382
Report Number: E-7479
Accession Number
73N28174
Funding Number(s)
PROJECT: RTOP 501-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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