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Numerical prediction of 3-D ejector flowsThe 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.
Document ID
19800001872
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Roberts, D. W.
(Boeing Military Airplane Development Seattle, WA, United States)
Paynter, G. C.
(Boeing Military Airplane Development Seattle, WA, 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
80N10111
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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