NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Application of computational fluid dynamics to complex inlet ductsA three-dimensional parabolic Navier-Stokes code, PEPSIG, was used to analyze the flow in the subsonic diffuser section of a typical modern inlet design. The effect of curvature of the diffuser centerline and transitioning cross sections was studied to determine the primary cause of flow distortion in the duct. Total pressure values at the engine compressor face are reported.
Document ID
19850021935
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Towne, C. E. (NASA Lewis Research Center Cleveland, OH, United States)
Schum, E. F. (Rockwell International Corp. Columbus, Ohio, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-87060
E-2629
NAS 1.15:87060
AIAA PAPER 85-1213
Report Number: NASA-TM-87060
Report Number: E-2629
Report Number: NAS 1.15:87060
Report Number: AIAA PAPER 85-1213
Meeting Information
Meeting: Joint Propulsion Conf.
Location: Monterey, CA
Country: United States
Start Date: July 8, 1985
End Date: July 10, 1985
Sponsors: AIAA, ASEE, SAE, ASME
Accession Number
85N30247
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available