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A computational model for three-dimensional incompressible wall jets with large cross flowA computational model for the flow field of three dimensional incompressible wall jets prototypic of thrust augmenting ejectors with large cross flow is presented. The formulation employs boundary layer equations in an orthogonal curvilinear coordinate system. Simulation of laminar as well as turbulen wall jets is reported. Quantification of jet spreading, jet growth, nominal separation, and jet shrink effects due to corss flow are discussed.
Document ID
19800001876
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Murphy, W. D. (Rockwell International Science Center Thousand Oaks, CA, United States)
Shankar, V. (Rockwell International Science Center Thousand Oaks, CA, United States)
Malmuth, N. D. (Rockwell International Science Center Thousand Oaks, CA, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1979
Publication Information
Publication: NASA. Ames Res. Center Workshop on Thrust Augmenting Ejectors
Subject Category
Aerodynamics
Accession Number
80N10115
Funding Number(s)
CONTRACT_GRANT: N62269-77-C-0412
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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