NASA NTRS · 19800001872
Numerical prediction of 3-D ejector flows
Abstract
The use of parametric flow analysis, rather than parametric scale testing, to support the design of an ejector system offers a number of potential advantages. The application of available 3-D flow analyses to the design ejectors can be subdivided into several key elements. These are numerics, turbulence modeling, data handling and display, and testing in support of analysis development. Experimental and predicted jet exhaust for the Boeing 727 aircraft are examined.
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Roberts, D. W., Paynter, G. C.. 1979-09-01. Numerical prediction of 3-D ejector flows. https://ntrs.nasa.gov/citations/19800001872
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