A sensitivity study on the effect of blade sweep on the trade-off between propeller efficiency and noise with panel method analysis

Master Thesis (2021)
Authors

T.H. Keil (TU Delft - Aerospace Engineering)

Faculty
Aerospace Engineering, Aerospace Engineering
Copyright
© 2021 Timo Keil
More Info
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Publication Year
2021
Language
English
Copyright
© 2021 Timo Keil
Graduation Date
27-10-2021
Awarding Institution
Delft University of Technology
Programme
Aerospace Engineering
Faculty
Aerospace Engineering, Aerospace Engineering
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Abstract

Due to increasing concerns on the environmental impact of aviation operations and rising fuel prices, there is renewed interest in propeller research. Although propellers can provide a step improvement in propulsive efficiency with respect to turbofan engines, they are generally associated with higher noise emissions. In this study, the effect of blade sweep on the trade-off between propeller efficiency and noise is investigated. A panel method was implemented to analyze the propeller aerodynamics, while a tonal far-field frequency formulation was used to analyze the propeller acoustics. It was concluded that the effect of blade sweep on the thickness noise for conventional propeller systems at a constant advance ratio is noticeable. A relation was found for the trade-off between propeller efficiency and noise. This relation shows that the sensitivity of noise reduction reduces as the maximum allowed efficiency penalty is increased.

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