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Title:

Unsteady Effects of the separated flow at the tail section of a helicopter fuselage

Document type:
Konferenzbeitrag
Contribution type:
Textbeitrag / Aufsatz
Author(s):
Vogel, F.; Breitsamter, C.; Adams, N.A.
Keywords:
helicopter fuselage
Dewey Decimal Classification:
620 Ingenieurwissenschaften
Book / Congress title:
European Rotorcraft Forum [35th]
Date of congress:
22.-25.9.
Year:
2009
Reviewed:
ja
Language:
en
TUM Institution:
Lehrstuhl für Aerodynamik
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