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Extensions and improvements on XTRAN3SImprovements to the XTRAN3S computer program are summarized. Work on this code, for steady and unsteady aerodynamic and aeroelastic analysis in the transonic flow regime has concentrated on the following areas: (1) Maintenance of the XTRAN3S code, including correction of errors, enhancement of operational capability, and installation on the Cray X-MP system; (2) Extension of the vectorization concepts in XTRAN3S to include additional areas of the code for improved execution speed; (3) Modification of the XTRAN3S algorithm for improved numerical stability for swept, tapered wing cases and improved computational efficiency; and (4) Extension of the wing-only version of XTRAN3S to include pylon and nacelle or external store capability.
Document ID
19890009865
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Borland, C. J.
(Boeing Military Airplane Development Seattle, WA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1989
Publication Information
Publication: NASA, Langley Research Center, Transonic Unsteady Aerodynamics and Aeroelasticity 1987, Part 1
Subject Category
Computer Programming And Software
Accession Number
89N19236
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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