- Standort
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Deutsche Nationalbibliothek Frankfurt am Main
- Umfang
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1 Online-Ressource.
- Sprache
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Englisch
- Erschienen in
-
Resolvent model for aeroacoustics of trailing edge noise ; volume:38 ; number:2 ; day:8 ; month:4 ; year:2024 ; pages:163-183 ; date:4.2024
Theoretical and computational fluid dynamics ; 38, Heft 2 (8.4.2024), 163-183, 4.2024
- Urheber
-
Demange, S.
Yuan, Z.
Jekosch, S.
Hanifi, A.
Cavalieri, A. V. G.
Sarradj, E.
Kaiser, T. L.
Oberleithner, K.
- Beteiligte Personen und Organisationen
-
SpringerLink (Online service)
- DOI
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10.1007/s00162-024-00688-z
- URN
-
urn:nbn:de:101:1-2408182125046.011915955638
- Rechteinformation
-
Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Letzte Aktualisierung
-
14.08.2025, 11:01 MESZ
Datenpartner
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Beteiligte
- Demange, S.
- Yuan, Z.
- Jekosch, S.
- Hanifi, A.
- Cavalieri, A. V. G.
- Sarradj, E.
- Kaiser, T. L.
- Oberleithner, K.
- SpringerLink (Online service)
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Self Noise Reduction and Aerodynamics of Airfoils with Porous Trailing Edges
Leading- and trailing-edge noise reduction using serrations of new geometry
Noise Reduction of a Centrifugal Plenum Fan with Leading Edge or Trailing Edge Serrations
Influence of rotor solidity on trailing edge noise from wind turbine blades
Design methodology for trailing-edge high-lift mechanisms
Investigation of blunt trailing edge noise from an asymmetric airfoil under different aerodynamic loads
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