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Procedures for the computation of unsteady transonic flows including viscous effectsModifications of the code LTRAN2, developed by Ballhaus and Goorjian, which account for viscous effects in the computation of planar unsteady transonic flows are presented. Two models are considered and their theoretical development and numerical implementation is discussed. Computational examples employing both models are compared with inviscid solutions and with experimental data. Use of the modified code is described.
Document ID
19820012270
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rizzetta, D. P.
(Boeing Military Airplane Development Seattle, WA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:166249
NASA-CR-166249
Report Number: NAS 1.26:166249
Report Number: NASA-CR-166249
Accession Number
82N20144
Funding Number(s)
PROJECT: RTOP 505-31-11
CONTRACT_GRANT: NAS2-10762
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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