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User's manual for XTRAN2L (version 1.2): A program for solving the general-frequency unsteady transonic small-disturbance equationThe development, use and operation of the XTRAN2L program that solves the two dimensional unsteady transonic small disturbance potential equation are described. The XTRAN2L program is used to calculate steady and unsteady transonic flow fields about airfoils and is capable of performing self contained transonic flutter calculations. Operation of the XTRAN2L code is described, and tables defining all input variables, including default values, are presented. Sample cases that use various program options are shown to illustrate operation of XTRAN2L. Computer listings containing input and selected output are included as an aid to the user.
Document ID
19860022061
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Seidel, D. A.
(NASA Langley Research Center Hampton, VA, United States)
Batina, J. T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:87737
NASA-TM-87737
Report Number: NAS 1.15:87737
Report Number: NASA-TM-87737
Accession Number
86N31533
Funding Number(s)
PROJECT: RTOP 505-63-21-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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