Effects of Leading-Edge Separation on the Vibroacoustic Signature of a Heaving Airfoil at Low Mach Number

AuthID
P-00N-T0K
1
Author(s)
Tipo de Documento
Proceedings Paper
Year published
2018
Publicado
in AIAA Aerospace Sciences Meeting, 2018
Número: 210059
Conference
Aiaa Aerospace Sciences Meeting, 2018, Date: 8 January 2018 through 12 January 2018
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Publication Identifiers
SCOPUS: 2-s2.0-85044401502
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