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A three-dimensional, compressible, laminar boundary-layer method for general fuselages. Volume 2: User's manualThis user's manual contains a complete description of the computer programs developed to calculate three-dimensional, compressible, laminar boundary layers for perfect gas flow on general fuselage shapes. These programs include the 3-D boundary layer program (3DBLC), the body-oriented coordinate program (BCC), and the streamline coordinate program (SCC). Subroutine description, input, output and sample case are discussed. The complete FORTRAN listings of the computer programs are given.
Document ID
19920015101
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wie, Yong-Sun (High Technology Corp. Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1990
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-4292-VOL-2
NAS 1.26:4292-VOL-2
Report Number: NASA-CR-4292-VOL-2
Report Number: NAS 1.26:4292-VOL-2
Accession Number
92N24344
Funding Number(s)
CONTRACT_GRANT: NAS1-18240
PROJECT: RTOP 505-60-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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