Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97071/1/AIAA2012-1842.pd
A methodology is developed to perform minimum weight structural design for composite or metallic mai...
Sectional stiffness properties of composite rotor blades, such as the axial, torsional, and bending ...
AbstractThe paper presents an analytical study of the helicopter rotor vibratory load reduction desi...
The development of structural models for composite rotor blades is summarized. The models are inten...
Composite material systems are currently good candidates for aerospace structures, primarily for the...
AbstractThe compatibility between a composite beam cross-sectional analysis based on the variational...
A modular structural design methodology for composite blades is developed. This design method can be...
The problem of vibration has limited the use of helicopters in both civil and military applications....
Composite material systems are currently candidates for aerospace structures, primarily for the desi...
Advanced composite materials provide a wide range of design freedom by virtue of their anisotropy. F...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76484/1/AIAA-2009-2601-797.pd
The results from an initial phase of an in-house study aimed at improving the dynamic and aerodynami...
AbstractThis study describes an integrated framework in which basic aerospace engineering aspects (p...
The development of theoretical rotor blade structural models for designs based upon composite constr...
Recent studies on rotor aeroelastic response and stability have shown the beneficial effects of inco...
A methodology is developed to perform minimum weight structural design for composite or metallic mai...
Sectional stiffness properties of composite rotor blades, such as the axial, torsional, and bending ...
AbstractThe paper presents an analytical study of the helicopter rotor vibratory load reduction desi...
The development of structural models for composite rotor blades is summarized. The models are inten...
Composite material systems are currently good candidates for aerospace structures, primarily for the...
AbstractThe compatibility between a composite beam cross-sectional analysis based on the variational...
A modular structural design methodology for composite blades is developed. This design method can be...
The problem of vibration has limited the use of helicopters in both civil and military applications....
Composite material systems are currently candidates for aerospace structures, primarily for the desi...
Advanced composite materials provide a wide range of design freedom by virtue of their anisotropy. F...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76484/1/AIAA-2009-2601-797.pd
The results from an initial phase of an in-house study aimed at improving the dynamic and aerodynami...
AbstractThis study describes an integrated framework in which basic aerospace engineering aspects (p...
The development of theoretical rotor blade structural models for designs based upon composite constr...
Recent studies on rotor aeroelastic response and stability have shown the beneficial effects of inco...
A methodology is developed to perform minimum weight structural design for composite or metallic mai...
Sectional stiffness properties of composite rotor blades, such as the axial, torsional, and bending ...
AbstractThe paper presents an analytical study of the helicopter rotor vibratory load reduction desi...
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