IOP Conference Series Materials Science and Engineering · 2015 · 23 citations · 6 references
EngineeringAerospace EngineeringAerodynamicsFluid DynamicsTunnel EngineeringAerodynamic DesignExperimental AerodynamicsLow-speed AerodynamicsSubsonic AerodynamicsTurbulent FlowWind-tunnel TestingOptimal DesignReynolds NumberReynolds Number Effects
The presence of wind tunnel is undoubtedly bringing infinite possibilities to studying and understanding complex fluid flows. However, commercial wind tunnel is expensive and only limited to highly-focus researchers or exclusive institutions. This paper discusses the design and development of a low-cost, educational-purposed, open-typed subsonic wind tunnel. In this work, an open-typed subsonic wind tunnel is designed with the aim of achieving turbulent intensity (in the working section) below or equal to 5%, within the budget of RM 1500 and a working speed of 6 m/s - 8 m/s to meet the Reynolds number in the order of 105. The conceptual design was studied using Ansys Fluent 14.5 and the optimal design was then developed and experimentally verified.
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Design rules for small low speed wind tunnels
Rabindra D. Mehta, P. Bradshaw · The Aeronautical Journal · 1979 · 398 citations
The design of low-speed wind tunnels
P. Bradshaw, R. C. Pankhurst · Progress in Aerospace Sciences · 1964 · 145 citations