Hollow design of engine turbine disk to minimize stress at blade fir tree

• المؤلف الرئيسي: Lee, Jian Ming
• مؤلفون آخرون: Chow Wai Tuck
• التنسيق: Final Year Project
• اللغة: English
• منشور في: Nanyang Technological University 2020
• الموضوعات: Engineering::Aeronautical engineering::Jet propulsion
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/140483
• المؤسسة: Nanyang Technological University

This report presents the study of the effects of a hollow design of the engine turbine disk to minimise stress at the disk-blade fir tree design. The study was first conducted using script programming with Mechanical ANSYS Parametric Design Language (MAPDL), to perform a gradient descent study and t...