K. Y. Maalawi’s scientific contributions

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Publications (1)


Fig. 1: Closed-section shell with arbitrary shape [7]
Fig. 3: Modeling of a tapered spar 
Fig. 6: Spanwise material grading of twenty-segment spar function fmincon is applied to most smooth objective functions with smooth constraints. It is the most suitable function to the optimization problem of this investigation.
Properties of constituent materials [1]
Actual dimensions (mm) and natural frequencies of the optimum spar
Dynamic Optimization of Thin-walled Composite Blades of Wind Turbines
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January 2015

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223 Reads

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2 Citations

World Applied Sciences Journal

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K. Y. Maalawi

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S. M. Abdrabbo

The design of thin-walled composite blades is optimized in order to provide high dynamic performance. The optimal design is originated with respect to maximum natural frequency criterion. The optimization model employs the concept of spanwise material grading along the blade axis. Spanwise material grading is achieved by changing the distribution of fiber volume fraction along the blade length. The main blade spar is represented by a beam composed of multiple uniform segments each of which has different cross-sectional properties and length. Transfer matrix technique is used to study the dynamic behavior of such a beam. Design variables are chosen to be the cross-section dimensions, length, fiber orientation angle and fiber volume fraction of each segment. The optimization problem is formulated analytically as non-linear constrained problem solved by sequential quadratic programming technique. Finite element modeling using NX Nastran solver is performed in order to validate the analytical results. The results show that the approach used in this study enhances the dynamic characteristics of the optimized blades as compared with a baseline design.

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Citations (1)


... In the reference blade of UH-60, the composite layer angle distributions are in the form of CUS configuration. For a thin-walled beam, researchers use CUS and CAS composite layup configurations [24][25][26][27][28], given in Fig. 5. In this study, helicopter rotor performance is optimized without any restriction as opposed to frequently used ply angle distributions. ...

Reference:

Helicopter rotor blade vibration reduction with optimizing the structural distribution of composite layers
Dynamic Optimization of Thin-walled Composite Blades of Wind Turbines

World Applied Sciences Journal