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Analysis of stratified and closely spaced jets exhausting into a crossflowProcedures have been developed for determining the flow field about jets with velocity stratification exhausting into a crossflow. Jets with three different types of exit velocity stratification have been considered: (1) jets with a relatively high velocity core; (2) jets with a relatively low velocity core; and (3) jets originating from a vaned nozzle. The procedure developed for a jet originating from a high velocity core nozzle is to construct an equivalent nozzle having the same mass flow and thrust but having a uniform exit velocity profile. Calculations of the jet centerline and induced surface static pressures have been shown to be in good agreement with test data for a high velocity core nozzle. The equivalent ideal nozzle has also been shown to be a good representation for jets with a relatively low velocity core and for jets originating from a vaned nozzle in evaluating jet-induced flow fields. For the singular case of a low velocity core nozzle, namely a nozzle with a dead air core, and for the vaned nozzle, an alternative procedure has been developed. The internal mixing which takes place in the jet core has been properly accounted for in the equations of motion governing the jet development. Calculations of jet centerlines and induced surface static pressures show good agreement with test data these nozzles.
Document ID
19740003005
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ziegler, H.
(Northrop Corp. Hawthorne, CA, United States)
Woller, P. T.
(Northrop Corp. Hawthorne, CA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1973
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-132297
NOR-73-77
Report Number: NASA-CR-132297
Report Number: NOR-73-77
Accession Number
74N11118
Funding Number(s)
CONTRACT_GRANT: NAS1-11524
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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