Computational Aeroacoustic Investigation of a Helicopter Configuration with Ducted Tail Rotor

Title:: Computational Aeroacoustic Investigation of a Helicopter Configuration with Ducted Tail Rotor
Document type:: Konferenzbeitrag
Contribution type:: Textbeitrag / Aufsatz
Author(s):: You, J.H.; Breitsamter, C.; Adams, N.A.
Keywords:: Computational Aeroacoustic Investigation; helicopter configuration; Ducted Tail Rotor
Dewey Decimal Classification:: 620 Ingenieurwissenschaften
Book / Congress title:: ANSYS Conference & 30. CADFEM Users´Meeting
Date of congress:: 24.-26.10.
Year:: 2012
Reviewed:: ja
Language:: en
TUM Institution:: Lehrstuhl für Aerodynamik
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