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XTRAN2L: A program for solving the general-frequency unsteady transonic small disturbance equationA program, XTRAN2L, for solving the general-frequency unsteady transonic small disturbance potential equation was developed. It is a modification of the LTRAN2-NLR code. The alternating-direction-implicit (ADI) method of Rizzetta and Chin is used to advance solutions of the potential equation in time Engquist-Osher monotone spatial differencing is used in the ADI solution algorithm. As a result, the XTRAN2L code is more robust and more efficient than similar codes that use Murman-Cole type-dependent spatial differencing. Nonreflecting boundary conditions that are consistent with the general-frequency equation have been developed and implemented at the far-field boundaries. Use of those conditions allow the computational boundaries to be moved closer to the airfoil with no loss of accuracy. This makes the XTRAN2L code more economical to use.
Document ID
19840005082
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Whitlow, W., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1983
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-85723
NAS 1.15:85723
Report Number: NASA-TM-85723
Report Number: NAS 1.15:85723
Accession Number
84N13150
Funding Number(s)
PROJECT: RTOP 505-33-43-09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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