Results of aeroacoustic wind tunnel measurements on 6 ultralight aircraft propellers (2-, 3-, 4-, and 6-blade) are presented. Thrust, torque, and sound-pressure measurements for helical Mach numbers 0.4 to 0.7 and propeller pitch angles 10 to 25 deg are included.
Data of Aeroacoustic Measurements on Ultralight Aircraft Propellers
1988
122 pages
Report
No indication
English
CFD AND AEROACOUSTIC ANALYSIS OFWINGTIP-MOUNTED PROPELLERS
British Library Conference Proceedings | 2020
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