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Some aspects of calculating flows about three-dimensional subsonic inletsVarious three dimensional inlet models were calculated based on the potential flow model. Results are presented in the forms of surface static pressure, flow angularity, surface flow pattern, and inlet flow field. It is indicated that the extension of the lower lip can reduce the adverse pressure gradient and increase the flow separation bound.
Document ID
19820017337
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kao, H. C. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-82789
E-941
NAS 1.15:82789
Accession Number
82N25213
Funding Number(s)
PROJECT: RTOP 505-42-62
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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