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FlinoviaFlow Induced Noise and Vibration Issues and AspectsIV 2024 ed. [Hardback]

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  • Formāts: Hardback, 354 pages, height x width: 235x155 mm, 207 Illustrations, color; 15 Illustrations, black and white; X, 354 p. 222 illus., 207 illus. in color., 1 Hardback
  • Izdošanas datums: 13-Feb-2025
  • Izdevniecība: Springer International Publishing AG
  • ISBN-10: 3031739345
  • ISBN-13: 9783031739347
  • Hardback
  • Cena: 198,63 €*
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  • Standarta cena: 233,69 €
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  • Formāts: Hardback, 354 pages, height x width: 235x155 mm, 207 Illustrations, color; 15 Illustrations, black and white; X, 354 p. 222 illus., 207 illus. in color., 1 Hardback
  • Izdošanas datums: 13-Feb-2025
  • Izdevniecība: Springer International Publishing AG
  • ISBN-10: 3031739345
  • ISBN-13: 9783031739347

This book gathers the latest advances and innovations in the field of flow-induced vibration and noise, as presented by leading international researchers at the 4th International Symposium on Flow-Induced Noise and Vibration Issues and Aspects (FLINOVIA), which was held in Sydney, Australia, in May 2023. It explores topics such as turbulent boundary layer-induced vibration and noise, noise due to ingested turbulence, rotor noise, fluid-structure interaction problems, innovative measurement methods, and noise control techniques. The authors’ backgrounds represent a mix of academia, government, and industry, and several papers include applications to important problems for underwater vehicles, aerospace applications, and commercial transportation. The book offers a valuable reference guide for all those interested in measurement, modelling, simulation, and reproduction of the flow excitation and flow-induced structural response.

Fluid-acoustic interactions with resonance around an axial fan in a
duct.- Porous edges for flow noise reduction from theory to
application.- Similitude Laws for Scaling Vibrations and Acoustic Radiation
of Panels Excited by a Turbulent Boundary Layer.- Validity of Amiets theory
on airfoil wall-pressure fluctuations subjected to turbulent
inflow.- Transient aeroacoustic analysis of pitching wing at low Reynolds
number.