This Website is not fully compatible with Internet Explorer.
For a more complete and secure browsing experience please consider using Microsoft Edge, Firefox, or Chrome

Practical Application of Torsional Buckling Analysis Methodology for Aeroengine Drive Shaft


This paper was presented at the 9th International NAFEMS World Congress, held from May 27th-31st in Orlando, Florida, USA.

Document Details

ReferenceNWC03_55
AuthorRobotham. W
LanguageEnglish
TypePaper
Date 27th May 2003
OrganisationUniversity of Nottingham

Download


Back to Previous Page