NASA NTRS · 19800001876
A computational model for three-dimensional incompressible wall jets with large cross flow
Abstract
A 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.
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Murphy, W. D., Shankar, V., Malmuth, N. D.. 1979-09-01. A computational model for three-dimensional incompressible wall jets with large cross flow. https://ntrs.nasa.gov/citations/19800001876
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