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Design and testing of a low subsonic wind tunnel gust generator
Advances in aircraft and spacecraft science
This paper summarises the design of a gust generator and the comparison between high fidelity numerical results and experimental results. The gust generator has been designed for a low subsonic wind tunnel in order to perform gust response experiments on wings and assess load alleviation. Special attention has been given to the different design parameters that influence the shape of the gust velocity profile by means of CFD simulations. Design parameters include frequency of actuation, flowdoi:10.12989/aas.2017.4.2.125 fatcat:lm33duyunfcchp3tv43bucndfi