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Studies of the effects of curvature on dilution jet mixingAn analytical program was conducted using both three-dimensional numerical and empirical models to investigate the effects of transition liner curvature on the mixing of jets injected into a confined crossflow. The numerical code is of the TEACH type with hybrid numerics; it uses the power-law and SIMPLER algorithms, an orthogonal curvilinear coordinate system, and an algebraic Reynolds stress turbulence model. From the results of the numerical calculations, an existing empirical model for the temperature field downstream of single and multiple rows of jets injected into a straight rectangular duct was extended to model the effects of curvature. Temperature distributions, calculated with both the numerical and empirical models, are presented to show the effects of radius of curvature and inner and outer wall injection for single and opposed rows of cool dilution jets injected into a hot mainstream flow.
Document ID
19920038455
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Holdeman, James D.
(NASA Lewis Research Center Cleveland, OH, United States)
Srinivasan, Ram
(NASA Lewis Research Center Cleveland, OH, United States)
Reynolds, Robert S.
(NASA Lewis Research Center Cleveland, OH, United States)
White, Craig D.
(Allied-Signal Aerospace Co. Phoenix, AZ, United States)
Date Acquired
August 15, 2013
Publication Date
February 1, 1992
Publication Information
Publication: Journal of Propulsion and Power
Volume: 8
ISSN: 0748-4658
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
92A21079
Distribution Limits
Public
Copyright
Other

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