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Trailing edge noise prediction based on wall pressure spectrum models for NACA0012 airfoil

Structurae cannot make the full text of this publication available at this time. The full text can be accessed through the publisher via the DOI: 10.1016/j.jweia.2018.01.030.
  • About this
    data sheet
  • Reference-ID
    10356098
  • Published on:
    13/08/2019
  • Last updated on:
    13/08/2019
 
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