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Research on free and impinging jets for the development of STOL aircraftThe effect of the exit plane conditions on the initial region of an axisymmetric jet was systematically investigated. An essentially top-hat mean velocity profile and a homogeneous turbulence structure were maintained at the exit plane for eight distinct scale and intensity conditions. Mass and momentum flux values are independent of the exit turbulence structure for the range investigated; however, a significant (approximately 25%) increase in the latter implies a pronounced static pressure decrement inside the jet. Details of the velocity profile and turbulence structure are influenced by the exit plane conditions. The three radial-axial components of the Reynolds stress tensor have been conditionally sampled and are analyzed to show the initial condition effects.
Document ID
19740011789
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Foss, J. F.
(Michigan State Univ. East Lansing, MI, United States)
Kleis, S. J.
(Michigan State Univ. East Lansing, MI, United States)
Date Acquired
September 3, 2013
Publication Date
January 21, 1974
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-138031
Report Number: NASA-CR-138031
Accession Number
74N19902
Funding Number(s)
CONTRACT_GRANT: NGR-23-004-068
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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