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- W2910112596 abstract "Wind tunnel gust generator is important experiment equipment for gust load alleviation of aircrafts, however, there is less investigation on flow field performance parameter of gust generator. To investigate a gust generator composed of NACA0018 airfoil cascades, two dimensions hot wire anemometry is utilized to measure the flow field with different condition in a low turbulence wind tunnel. To estimate the performance parameter of flow field, online angle correction is used for improving the accuracy and efficiency of the two dimensions hot wire probe, phase analysis method is used for calculating the amplitude and fluctuation of periodic gust. The experiment of gust generator shows that, gust amplitude has a proportional relation with the NACA0018 airfoil oscillation frequency in range of 4Hz~15Hz, oscillation angle in range of 8°~30°, chord length in range of 50mm~100mm. Non-stability(velocity fluctuation at same phase) of gust flow has some linearity relation with oscillation angle and wind speed, which increases along with oscillation angle and wind speed in our test range, at the same time, proper oscillation frequency can decrease non-stability. The conclusion is helpful for gust generator research and flow field measurement in wind tunnel." @default.
- W2910112596 created "2019-01-25" @default.
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- W2910112596 date "2018-07-01" @default.
- W2910112596 modified "2023-09-27" @default.
- W2910112596 title "Investigation on Gust Generator Experiment with Two Dimensions Hot Wire Anemometry" @default.
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- W2910112596 doi "https://doi.org/10.1109/icisce.2018.00236" @default.
- W2910112596 hasPublicationYear "2018" @default.
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