Aeroacoustic characteristics of single propeller-wing configuration
收藏DataCite Commons2024-07-27 更新2024-07-13 收录
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https://data.bris.ac.uk/data/dataset/2g1tj1igqpola23r2x2l0lxyg9/
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资源简介:
The measurements were taken in the University of Bristol’s aeroacoustic wind tunnel facility. The five-bladed propeller with a diameter of D = 9” and P/D = 1 was mounted in the centre of the NACA0018 wing to create a case where the wake from the propellers impinge directly on the wing to investigate the effects of propeller-wing interaction at various advance ratios while maintaining a constant rotational speed of Ω = 8000 rpm.
提供机构:
University of Bristol
创建时间:
2023-12-08



