Taiwan / United States
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Construction of Numerical Wind Tunnel Based on Design Procedure: From Aircraft Geometric Definition To Aircraft Flow Solutions
The Numerical Wind Tunnel (NWT) is a high-performance computational system dedicated to CFD solutions of an industrial scale. It enables users to easily and efficiently compute, manage growing data, visualize the results in real time, and devise engineering designs. For SC’98, NWT is applied to a conceptually designed inter-island small business aircraft.
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Contact
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Fang-Pang Lin
National Center for High-Performance Computing
Taiwan
c00fpl00@nchc.gov.tw
(note: the “l” is the lower case of “L”)
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Collaborators
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Fang-Pang Lin, Ren-Jieh Shih, San-Liang Chu, Alpha Wang, Mei-Ling Hsu, Charlie H. Chang, Kuo-Wei Wu
National Center for High-Performance Computing
Taiwan
Donglong Sheu
National Cheng Kung University
Taiwan
Da-Pan Chen
National Chioa-Tung University
Taiwan
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www.nchc.gov.tw/RESEARCH/NWT
www.nchc.gov.tw/RESEARCH/CFDEE/Publications/index.html
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