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PROFILE: Airfoil Geometry Manipulation and DisplayThis report provides user information for program PROFILE, an aerodynamics design utility for plotting, tabulating, and manipulating airfoil profiles. A dozen main functions are available. The theory and implementation details for two of the more complex options are also presented. These are the REFINE option, for smoothing curvature in selected regions while retaining or seeking some specified thickness ratio, and the OPTIMIZE option, which seeks a specified curvature distribution. Use of programs QPLOT and BPLOT is also described, since all of the plots provided by PROFILE (airfoil coordinates, curvature distributions, pressure distributions)) are achieved via the general-purpose QPLOT utility. BPLOT illustrates (again, via QPLOT) the shape functions used by two of PROFILE's options. These three utilities should be distributed as one package. They were designed and implemented for the Applied Aerodynamics Branch at NASA Ames Research Center, Moffett Field, California. They are all written in FORTRAN 77 and run on DEC and SGI systems under OpenVMS and IRIX.
Document ID
19970011044
Acquisition Source
Ames Research Center
Document Type
Contractor Report (CR)
Authors
Collins, Leslie
(Sterling Software, Inc. Redwood Shores, CA United States)
Saunders, David
(Sterling Software, Inc. Redwood Shores, CA United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1997
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-177332
A-976001
NAS 1.26:177332
Report Number: NASA-CR-177332
Report Number: A-976001
Report Number: NAS 1.26:177332
Accession Number
97N16093
Funding Number(s)
CONTRACT_GRANT: NAS2-13210
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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