An experimental investigation of the aeroacoustic of propeller at low speeds

Guo Qing Zhang*, Shu Xing Yang, Song Hai Xue

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Citation (Scopus)

Abstract

The aeroacoustic characteristics of propeller-wing were simulated numerically. And the efficiency affected by the installation of angle of the propeller blade was also analyzed. Based on the pressure cloud and streamlines, This experiment used FW-H equation proposed by Ffowcs Williams and Hawkings to imitate the sound generation and dissemination.

Original languageEnglish
Title of host publicationProceedings - 2010 2nd International Conference on Modeling, Simulation, and Visualization Methods, WMSVM 2010
Pages197-202
Number of pages6
DOIs
Publication statusPublished - 2010
Event2010 2nd International Conference on Modeling, Simulation, and Visualization Methods, WMSVM 2010 - Sanya, Hainan, China
Duration: 15 May 201016 May 2010

Publication series

NameProceedings - 2010 2nd International Conference on Modeling, Simulation, and Visualization Methods, WMSVM 2010

Conference

Conference2010 2nd International Conference on Modeling, Simulation, and Visualization Methods, WMSVM 2010
Country/TerritoryChina
CitySanya, Hainan
Period15/05/1016/05/10

Keywords

  • Aeroacoustic
  • Grid
  • Propeller
  • Sliding mesh
  • UAV

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