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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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