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Study of the TRAC Airfoil Table Computational SystemThe report documents the study of the application of the TRAC airfoil table computational package (TRACFOIL) to the prediction of 2D airfoil force and moment data over a wide range of angle of attack and Mach number. The TRACFOIL generates the standard C-81 airfoil table for input into rotorcraft comprehensive codes such as CAM- RAD. The existing TRACFOIL computer package is successfully modified to run on Digital alpha workstations and on Cray-C90 supercomputers. A step-by-step instruction for using the package on both computer platforms is provided. Application of the newer version of TRACFOIL is made for two airfoil sections. The C-81 data obtained using the TRACFOIL method are compared with those of wind-tunnel data and results are presented.
Document ID
19990047443
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Hu, Hong
(Hampton Univ. VA United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1999
Subject Category
Aeronautics (General)
Report/Patent Number
NAS 1.26:209323
NASA/CR-1999-209323
Report Number: NAS 1.26:209323
Report Number: NASA/CR-1999-209323
Funding Number(s)
CONTRACT_GRANT: NAS1-19935
PROJECT: RTOP 538-07-14-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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