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TAWFIVE: A user's guideThe Transonic Analysis of a Wing and Fuselage with Interacted Viscous Effects (TAWFIVE) was developed. A finite volume full potential method is used to model the outer inviscid flow field. First-order viscous effects are modeled by a three dimensional integral boundary layer method. Both turbulent and laminar boundary layers are treated. Wake thickness and curvature effects are modeled using a two dimensional strip method. A very brief discussion of the engineering aspects of the program is given. The input and use of the program are covered in great detail.
Document ID
19830027046
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Melson, N. D. (NASA Langley Research Center Hampton, VA, United States)
Streett, C. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1983
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-84619
NAS 1.15:84619
Report Number: NASA-TM-84619
Report Number: NAS 1.15:84619
Accession Number
83N35317
Funding Number(s)
PROJECT: RTOP 505-31-03-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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