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TRANDESNF: A computer program for transonic airfoil design and analysis in nonuniform flowThe use of a transonic airfoil code for analysis, inverse design, and direct optimization of an airfoil immersed in propfan slipstream is described. A summary of the theoretical method, program capabilities, input format, output variables, and program execution are described. Input data of sample test cases and the corresponding output are given.
Document ID
19870005753
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chang, J. F. (Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Lan, C. Edward (Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:4044
KU-FRL-602-1
NASA-CR-4044
Accession Number
87N15186
Funding Number(s)
CONTRACT_GRANT: NAG1-308
PROJECT: RTOP 535-03-01-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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