Torun, Ahmet Refah2025-01-062025-01-0620201222-534710.35530/IT.071.05.17172-s2.0-85096238333https://doi.org/10.35530/IT.071.05.1717https://hdl.handle.net/20.500.14669/3203Aerodynamic parts such as rocket nose and heat shield related composites are mainly produced with filament winding machines. Winding angle of the reinforcement filament is the main parameter to determine the thermomechanical properties of the final composite part. The angle adjustments on the machine cause the temporary response of the filaments. This study derives an analytical method to determine the real angle of the filaments on the mandrel.eninfo:eu-repo/semantics/openAccesswinding anglefilament windingcomposite materialsconical partscomplex shape mandrelsArticle4575Q345271WOS:000586533900007Q4