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Square-section prism with rounded edges in a uniform cross-flow: Effect of incidence angle and Reynolds number on the (un)steady aerodynamics and proneness to galloping

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.2024.105993.
  • About this
    data sheet
  • Reference-ID
    10809651
  • Published on:
    07/01/2025
  • Last updated on:
    07/01/2025
 
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