Recommendations on Dynamic Pressure Sensor Placement for Transonic Wind Tunnel Tests
A wind tunnel test was conducted which measured surface fluctuating pressures aft of a ramp at transonic speeds. Dynamic pressure test data was used to perform a study to determine best locations for streamwise sensor pairs for shocked and unshocked runs based on minimizing the error
in root-mean-square acceleration response of the panel. Recommendations are given for sensor pair locations for both shocked and unshocked runs.
Keywords: aeroacoustic; launch vehicle; test; transducer; transonic; vibroacoustic; wind tunnel
Document Type: Research Article
Publication date: 01 December 2018
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