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this work focuses on, these aerodynamic interactions are due to the main rotor wake impinging on the tail rotor for certain operating conditions that depend on vehicle design characteristics
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to enlist the main elastic and thermal properties. Later, the experiments will be performed and results will be analysed to empirically relate the elastic and thermal behaviour of the selected material
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performance degradations and unwarranted system failures can occur. There is certain physical information known a priori in such aerospace platform operations. The main research hypothesis to be tested in
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