Prediction of critical configurations of helicopter - external slung load system using bifurcation theory and continuation methods

Thumbnail Image

Files

22_13.PDF (1.92 MB)

Date

2000

Authors

Journal Title

Journal ISSN

Volume Title

Publisher

Abstract

Description

Keywords

Citation

URI

http://hdl.handle.net/20.500.11881/479

Collections

Papers

Endorsement

Review

Supplemented By

Referenced By