Use of bifurcation and continuation methods in the identification and control of aeroelastic induced effects on flexible aircraft dynamics

MN Baghdadi, MH Lowenberg, AT Isikveren

Research output: Chapter in Book/Report/Conference proceedingConference Contribution (Conference Proceeding)

Translated title of the contributionUse of bifurcation and continuation methods in the identification and control of aeroelastic induced effects on flexible aircraft dynamics
Original languageEnglish
Title of host publication51st AIAA/ASEM/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Publication statusPublished - Apr 2010

Bibliographical note

Name and Venue of Event: 18th AIAA/ASME/AHS Adaptive Structures Conference, Orlando, USA
Conference Organiser: AIAA

Cite this