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Some aspects of calculating flows about three-dimensional subsonic inletsBased on the potential flow model, computations were carried out for various three-dimensional inlet models. Some of these calculated results are presented in the forms of surface static pressure, flow angularity, surface flow pattern, and inlet flow field. Comparisons with experimental data are also made.
Document ID
19810019516
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-82678
E-941
Report Number: NASA-TM-82678
Report Number: E-941
Meeting Information
Meeting: Joint Propulsion Conf.
Location: Colorado Springs, CO
Country: United States
Start Date: July 27, 1981
End Date: July 29, 1981
Sponsors: ASME, AIAA, SAE
Accession Number
81N28054
Funding Number(s)
PROJECT: RTOP 505-42-62
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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