Experimental Study of the Effect of Boundary-Layer Transition on Rotor Aeroacoustics

  • Xiangtian Li
  • , Han Wu
  • , Yuhong Li
  • , Peng Zhou
  • , Siyang Zhong
  • , Zhaokai Ma

Research output: Journal article publicationComment/debate/erratum

6 Citations (Scopus)
Original languageEnglish
Pages (from-to)1974-1981
Number of pages8
JournalAIAA Journal
Volume62
Issue number5
DOIs
Publication statusPublished - May 2024

Keywords

  • Acoustic Measurement
  • Boundary Layer Transition
  • Free Stream Velocity
  • Heat Transfer Coefficients
  • Overall Sound Pressure Level
  • Research Facilities and Instrumentation
  • Rotor Aerodynamics
  • Rotor Blades

ASJC Scopus subject areas

  • Aerospace Engineering

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