Refer the book "Gas Turbine Powerhouse: The Development of the Power Generation Gas Turbine at BBC-ABB-Alstom" by Dietrich Eckardt (available at https://books.google.com/). On page 275 a reference of GT8 rotor damage due to high slenderness ratio is given. I could not find much about such effect in open literature. Does anybody know what is effect of rotor slenderness ratio (L/D) (or rotating body in general-any papers/references)? Few more specific questions:
Regards
Naveen Bhatt