年間 6 号発行
ISSN 印刷: 1948-2590
ISSN オンライン: 1948-2604
OPTIMAL AEROACOUSTIC PROPELLER DESIGN
要約
The main points of an aeroacoustic design method for single and coaxial propellers with a given number of blades and with some of their dimensionless geometric characteristics are presented. The results of noise level minimization near the propeller are presented under a number of restrictions in the range of the control parameters, flight efficiency, propeller thrust at the start and at take-off, reverse thrust, and propeller mass.
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A. Moshkov P., F. Samokhin V., A. Yakovlev A., Engine-propeller power plant aircraft community noise reduction key methods, 1952, 2018. Crossref
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Moshkov P. A., Samokhin V. F., Evaluation of the influence of the number of blades and diameter on propeller noise, VESTNIK of Samara University. Aerospace and Mechanical Engineering, 15, 3, 2016. Crossref