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A new experimental technique for roll damping moment evaluation is developed considering forced rotation method, the obtained results are compared with data obtained by free rotation method. Also, a correction method is developed for geometry deviation correction. A numerical study is performed for solver calibration and validation with experimental data. The results obtained from experimental testing and numerical simulations are compared with calibration data available.

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This page is a summary of: Roll Damping Measurements on Basic Finner Model Using Both Forced and Free Methods, Journal of Spacecraft and Rockets, June 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a35687.
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