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Document type:
Konferenzbeitrag 
Contribution type:
Textbeitrag / Aufsatz 
Author(s):
You, J.H.; Breitsamter, C.; Adams, N.A. 
Title:
Computational Aeroacoustic Investigation of a Helicopter Configuration with Ducted Tail Rotor 
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