DocumentCode
3734553
Title
Integrated design process for subsonic open circuit wind tunnel from empirical studies to CFD simulation
Author
T. H. H. Le;C. C. Nguyen;D. K. Le;N. D. Bui;N. H. Nguyen
Author_Institution
Department of Aerospace Engineering, Ho Chi Minh City University of Technology, Ho Chi Minh City, Vietnam
fYear
2015
Firstpage
99
Lastpage
104
Abstract
This paper proposes a process of determining geometrical configurations to simulating the flow in designing sub-sonic open circuit wind tunnels. Design rules that are based on empirical results and Computational Fluid Dynamics (CFD) model are integrated as a Low-Speed Wind Tunnel Design Tool. The tool allows users to undertake the automatic calculation through wind tunnel designed requirements to detailed flow fields analysis. Three configurations with the overall length of 7 to 10 meters and width from 3.5 to 4.2 meters are suggested. The design wind tunnels have the test section (cross section) of 1.7 × 1.7 meters squared and the test section velocity of 15 meters per second. The simulation results help to choose the best-designed wind tunnel configuration for manufacturing in the future.
Keywords
"Computational fluid dynamics","Mathematical model","Geometry","Design tools","Testing","Integrated circuit modeling","Computational modeling"
Publisher
ieee
Conference_Titel
Advanced Technologies for Communications (ATC), 2015 International Conference on
ISSN
2162-1020
Print_ISBN
978-1-4673-8372-1
Type
conf
DOI
10.1109/ATC.2015.7388426
Filename
7388426
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