Sectional stiffness properties of composite rotor blades, such as the axial, torsional, and bending stiffness, play an important role in the design and analysis of rotorcraft, as they impact the predicted rotor dynamics, structural loads, and stress and strain fields. Multiple numerical tools exist for predicting the sectional stiffness properties based on the cross-sectional geometries and materials; however, rotor blades are often made of composite materials and require complex manufacturing procedures, making it challenging to provide an accurate prediction of the inputs needed for these numerical tools. This dissertation therefore focuses on developing an experimental technique for calculating the sectional stiffness properties, based o...
Composite material systems are currently candidates for aerospace structures, primarily for the desi...
A study was conducted to demonstrate experimental identification of the structural properties of an ...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989....
Among all strain measurement techniques, digital image correlation is preferred over others because ...
The results from an initial phase of an in-house study aimed at improving the dynamic and aerodynami...
Recent studies on rotor aeroelastic response and stability have shown the beneficial effects of inco...
Structural deformation of composite wind turbine blades affect the aerodynamic performance of the ro...
The development of structural models for composite rotor blades is summarized. The models are inten...
A novel passive twist morphing concept is examined for helicopter blades. The concept is demonstrate...
The present study performs a set of static tests to demonstrate a novel passive morphing concept. Th...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97071/1/AIAA2012-1842.pd
AbstractThe compatibility between a composite beam cross-sectional analysis based on the variational...
Incorporating uncertainties in the aeroelastic analysis increases the confidence levels of computati...
The development of theoretical rotor blade structural models for designs based upon composite constr...
This study investigates the effect of uncertainty in composite material properties on the cross-sect...
Composite material systems are currently candidates for aerospace structures, primarily for the desi...
A study was conducted to demonstrate experimental identification of the structural properties of an ...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989....
Among all strain measurement techniques, digital image correlation is preferred over others because ...
The results from an initial phase of an in-house study aimed at improving the dynamic and aerodynami...
Recent studies on rotor aeroelastic response and stability have shown the beneficial effects of inco...
Structural deformation of composite wind turbine blades affect the aerodynamic performance of the ro...
The development of structural models for composite rotor blades is summarized. The models are inten...
A novel passive twist morphing concept is examined for helicopter blades. The concept is demonstrate...
The present study performs a set of static tests to demonstrate a novel passive morphing concept. Th...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97071/1/AIAA2012-1842.pd
AbstractThe compatibility between a composite beam cross-sectional analysis based on the variational...
Incorporating uncertainties in the aeroelastic analysis increases the confidence levels of computati...
The development of theoretical rotor blade structural models for designs based upon composite constr...
This study investigates the effect of uncertainty in composite material properties on the cross-sect...
Composite material systems are currently candidates for aerospace structures, primarily for the desi...
A study was conducted to demonstrate experimental identification of the structural properties of an ...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989....