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A numerical analysis applied to high angle of attack three-dimensional inletsThe three-dimensional analytical methods used to analyze subsonic high angle of attack inlets are described. The methods are shown to be in good agreement with experimental results for various three-dimensional high angle of attack inlets. The methods are used to predict aerodynamic characteristics of scarf and slotted-lip inlets.
Document ID
19860015187
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hwang, D. P. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:87298
AIAA PAPER 86-1627
NASA-TM-87298
E-3004
Report Number: NAS 1.15:87298
Report Number: AIAA PAPER 86-1627
Report Number: NASA-TM-87298
Report Number: E-3004
Meeting Information
Meeting: Joint Propulsion Conference
Location: Huntsville, AL
Country: United States
Start Date: June 16, 1986
End Date: June 18, 1986
Sponsors: ASME, ASEE, AIAA, SAE
Accession Number
86N24658
Funding Number(s)
PROJECT: RTOP 505-62-91
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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