Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76201/1/AIAA-2006-1821-974.pd
The problem of vibration has limited the use of helicopters in both civil and military applications....
Described is a formal optimization procedure for helicopter rotor blade design which minimizes hover...
The vibration and performance optimization procedure using regression analysis was successfully appl...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77207/1/AIAA-2006-6997-436.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77383/1/AIAA-40291-933.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77357/1/AIAA-2007-1898-902.pd
Design optimisation of a helicopter rotor blade is performed. The objective is to reduce helicopter ...
This dissertation describes an active/passive approach to optimum design of helicopter rotor blades ...
AbstractThe paper addresses the integration of blade dynamics, aerodynamics, structures and aeroelas...
The development and validation of an optimization procedure to systematically place tuning masses al...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76405/1/AIAA-2008-2178-413.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76484/1/AIAA-2009-2601-797.pd
Results of analytical investigations to develop, understand, and evaluate potential helicopter vibra...
A robust aeroelastic optimization is performed to minimize helicopter vibration with uncertainties i...
The importance of blade design parameters in rotor vibratory response and the design of a minimum vi...
The problem of vibration has limited the use of helicopters in both civil and military applications....
Described is a formal optimization procedure for helicopter rotor blade design which minimizes hover...
The vibration and performance optimization procedure using regression analysis was successfully appl...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77207/1/AIAA-2006-6997-436.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77383/1/AIAA-40291-933.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77357/1/AIAA-2007-1898-902.pd
Design optimisation of a helicopter rotor blade is performed. The objective is to reduce helicopter ...
This dissertation describes an active/passive approach to optimum design of helicopter rotor blades ...
AbstractThe paper addresses the integration of blade dynamics, aerodynamics, structures and aeroelas...
The development and validation of an optimization procedure to systematically place tuning masses al...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76405/1/AIAA-2008-2178-413.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76484/1/AIAA-2009-2601-797.pd
Results of analytical investigations to develop, understand, and evaluate potential helicopter vibra...
A robust aeroelastic optimization is performed to minimize helicopter vibration with uncertainties i...
The importance of blade design parameters in rotor vibratory response and the design of a minimum vi...
The problem of vibration has limited the use of helicopters in both civil and military applications....
Described is a formal optimization procedure for helicopter rotor blade design which minimizes hover...
The vibration and performance optimization procedure using regression analysis was successfully appl...
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