32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference 2016
DOI: 10.2514/6.2016-3656
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The Overall Scheme Design and Debugging of the Liquid Nitrogen Injection Cooling System in NF-6 Wind Tunnel

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“…The free-stream turbulence intensity of the wind tunnel is less than 0.15% at free-stream velocity u ∞ <136 m s −1 . The two-dimensional test section is 0.8 m×0.4 m in cross-section and 3 m in length, the schematic diagram of the wind tunnel was described in [25]. A two-dimensional NACA 0012 airfoil made of solid steel with a chord length c=200 mm and a span length of 400 mm was used as the test model.…”
Section: Methodsmentioning
confidence: 99%
“…The free-stream turbulence intensity of the wind tunnel is less than 0.15% at free-stream velocity u ∞ <136 m s −1 . The two-dimensional test section is 0.8 m×0.4 m in cross-section and 3 m in length, the schematic diagram of the wind tunnel was described in [25]. A two-dimensional NACA 0012 airfoil made of solid steel with a chord length c=200 mm and a span length of 400 mm was used as the test model.…”
Section: Methodsmentioning
confidence: 99%