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Design and performance evaluation for finalized active tab drive mechanism installed in Mach scaled model blade
Noboru, K.
(
2013
)
Simulation of main rotor noise emission generated due to blade thickness
Mirgazov, R.M.
;
Golovkin, V.A.
;
Kritsky, B.S.
(
2013
)
Prediction of noise reduction by an active flap of a model rotor
Tanabe, Y.
;
Kobiki, N.
;
Suguwara, H.
(
2013
)
Acoustic design and testing of the Eurocopter EC145T2 and EC175B - A harmonized Franco-German approach
Gareton, V.
;
Gervais, M.
;
Heger, R.
(
2013
)
Validation of aerodynamic and aeroacoustic computations of a Fenestron in real flight conditions
Gardarein, P.
;
Falissardi, F.
;
Binet, L.
;
Camus, J.-C.
(
2010
)
The effect of fuselage and rotor hub on blade-vortex interaction airloads and rotor wakes
Lim, J.W.
;
Dimanlig, A.C.B.
(
2010
)
Uncertainty quantification of noise abatement flight procedures
Olsman, W.F.J.
(
2015
)
Main rotor aeroacoustic analysis & validation with test data and favorable planform design for minimal aerodynamic noise
Yücekayali, A.
;
Senipek, M.
;
Ortakaya, Y.
(
2015
)
Design, analysis and prototyping of active tab rotor
Kobiki, N.
;
Tanabe, Y.
;
Aoyama, T.
;
Kim, D.-H.
;
Kang, H.J.
;
Wie, S.-Y.
;
Kim, S.-H.
(
2015
)
ANCORA: Anotec-Comoti rotorcraft acoustics initiative for preliminary acoustic flight tests for the tuning of simplified rotorcraft noise models
Van Oosten, N.
;
Dragasanu, L.
;
Cenedese, F.
(
2015
)
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Author
Gennaretti, M. (3)
Haase, T. (3)
Simon, F. (3)
Bernardini, G. (2)
Heger, R. (2)
Kobiki, N. (2)
Redaelli, M. (2)
Rolando, A. (2)
Tanabe, Y. (2)
Trainelli, L. (2)
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Acoustics (23)
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Date Issued
2016 (13)
2015 (4)
2013 (4)
2010 (2)