Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76119/1/AIAA-2005-2245-352.pd
A collaborative flight test programme was conducted to study among other objectives the potential of...
Combined variable rotor speed and active blade twist helicopter technologies have the potential to r...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76405/1/AIAA-2008-2178-413.pd
This work presents the development and application of an active control approach for reduction of bo...
This dissertation describes the development of a comprehensive aeroelastic/aeroacoustic simulation c...
This dissertation describes the development of a comprehensive aeroelastic/aeroacoustic simulation c...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76792/1/AIAA-2003-1785-854.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76329/1/AIAA-2006-1861-222.pd
Because of their peculiar ability to take off vertically and their excellent handling qualities in h...
Abstract A computational study of helicopter vibration and rotor shaft power reduction is conducted ...
An acoustics parametric analysis of the effect of fuselage drag and pitching moment on the Blade-Vor...
Helicopter-blade-vortex interaction noise is one of the most severe noise sources and is very import...
Helicopters suffer from severe vibration levels compared to fixed-wing aircraft. The main source of ...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/143060/1/6.2017-1179.pd
The present work focuses on the alleviation of Blade Vortex Interaction (BVI) noise annoyance throug...
A collaborative flight test programme was conducted to study among other objectives the potential of...
Combined variable rotor speed and active blade twist helicopter technologies have the potential to r...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76405/1/AIAA-2008-2178-413.pd
This work presents the development and application of an active control approach for reduction of bo...
This dissertation describes the development of a comprehensive aeroelastic/aeroacoustic simulation c...
This dissertation describes the development of a comprehensive aeroelastic/aeroacoustic simulation c...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76792/1/AIAA-2003-1785-854.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76329/1/AIAA-2006-1861-222.pd
Because of their peculiar ability to take off vertically and their excellent handling qualities in h...
Abstract A computational study of helicopter vibration and rotor shaft power reduction is conducted ...
An acoustics parametric analysis of the effect of fuselage drag and pitching moment on the Blade-Vor...
Helicopter-blade-vortex interaction noise is one of the most severe noise sources and is very import...
Helicopters suffer from severe vibration levels compared to fixed-wing aircraft. The main source of ...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/143060/1/6.2017-1179.pd
The present work focuses on the alleviation of Blade Vortex Interaction (BVI) noise annoyance throug...
A collaborative flight test programme was conducted to study among other objectives the potential of...
Combined variable rotor speed and active blade twist helicopter technologies have the potential to r...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76405/1/AIAA-2008-2178-413.pd
DOI
Add to ORKG