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

2 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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