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http://dx.doi.org/10.5139/JKSAS.2007.35.8.685

Development of GUI Program for Automated Generation of Airfoil Performance Table  

Kim, Tae-Woo (부산대학교 항공우주공학과 대학원)
Lee, Jae-Won (부산대학교 항공우주공학과 대학원)
Chae, Sang-Hyun (부산대학교 항공우주공학과 대학원)
Oh, Se-Jong (부산대학교 항공우주공학과)
Yee, Kwan-Jung (부산대학교 항공우주공학과)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.35, no.8, 2007 , pp. 685-692 More about this Journal
Abstract
This paper describes the development procedure of GUI Program for the automated generation of airfoil performance table used in helicopter comprehensive code. Considering commercialization, the program is developed based on the Windows operating system. In addition, it is aimed to enhance user's convenience by including embedded postprocessor which enables real-time display of calculation procedure and grid system. Using the validated CFD code, the aerodynamic analyses are automated for a given range of Mach number and angles of attack. The computational grid system is designed to generate automatically once the surface coordinates are given. Mixed-Language scheme is employed in order to combine the CFD code in Fortran with C++ based GUI program, which makes the time-consuming code conversion unnecessary.
Keywords
Computational Fluid Dynamics; Airfoil Aerodynamic Analysis; Graphic User Interface; Automatic Analysis; Rotor Blades;
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