Abstract:Systems of differential equations in cartesian and cylindrical coordinates are obtained to describe a fl exible fi lament rotating in a resisting medium. The concept of the unit aerodynamic drag coeffi cient of the fi lament is introduced in addition to the assumptions used in previous studies. The systems of differential equations that were obtained are solved in analytical form using the assumptions that were made. A value is found for the new concept of unit aerodynamic drag coeffi cient, and ways are descr… Show more
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