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An installed nacelle design code using a multiblock Euler solver. Volume 2: User guideThis is a user manual for the general multiblock Euler design (GMBEDS) code. The code is for the design of a nacelle installed on a geometrically complex configuration such as a complete airplane with wing/body/nacelle/pylon. It consists of two major building blocks: a design module developed by LaRC using directive iterative surface curvature (DISC); and a general multiblock Euler (GMBE) flow solver. The flow field surrounding a complex configuration is divided into a number of topologically simple blocks to facilitate surface-fitted grid generation and improve flow solution efficiency. This user guide provides input data formats along with examples of input files and a Unix script for program execution in the UNICOS environment.
Document ID
19920022984
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chen, H. C.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:189652-VOL-2
NASA-CR-189652-VOL-2
Report Number: NAS 1.26:189652-VOL-2
Report Number: NASA-CR-189652-VOL-2
Accession Number
92N32228
Funding Number(s)
CONTRACT_GRANT: NAS1-18703
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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