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NASA NTRS ยท 19990047443

Study of the TRAC Airfoil Table Computational System

Abstract

The 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.

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BibTeXRIS

Hu, Hong. 1999-05-01. Study of the TRAC Airfoil Table Computational System. https://ntrs.nasa.gov/citations/19990047443

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