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Aeroacoustic characteristics of single propeller-wing configuration

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.

Complete download (zip, 55.6 MiB)

Creator(s) Mahdi Azarpeyvand, Buda Turhan, Djamel Rezgui, Hasan Kamliya Jawahar, Luke Bowen
Publication date 08 Dec 2023
Language eng
Publisher University of Bristol
Licence Non-Commercial Government Licence for public sector information
DOI 10.5523/bris.2g1tj1igqpola23r2x2l0lxyg9
Citation Mahdi Azarpeyvand, Buda Turhan, Djamel Rezgui, Hasan Kamliya Jawahar, Luke Bowen (2023): Aeroacoustic characteristics of single propeller-wing configuration. https://doi.org/10.5523/bris.2g1tj1igqpola23r2x2l0lxyg9
Total size 55.6 MiB

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