Flap-lag stability of helicopter rotor blades using continuation and bifurcation methods

D Rezgui; MH Lowenberg; PC Bunniss

Flap-lag stability of helicopter rotor blades using continuation and bifurcation methods

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

Translated title of the contribution	Flap-lag stability of helicopter rotor blades using continuation and bifurcation methods
Original language	English
Title of host publication	3rd International Conference on Dynamics, Vibration & Control, Hangzhou, China
Publication status	Unpublished - May 2010

Bibliographical note

Name and Venue of Event: Mini-Symposium 13: Flight Dynamics & Control
Conference Organiser: The Chinese Society of Theoretical and Applied Mechanics (CSTAM)

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Persistent link

The 3rd International Conference on Dynamics, Vibration and Control (ICDVC)
Rezgui, D. (Speaker)
12 May 2010 → 14 May 2010
Activity: Participating in or organising an event types › Participation in conference

Cite this

@inproceedings{4c654f1be6064de38d66ffbe537b08e7,

title = "Flap-lag stability of helicopter rotor blades using continuation and bifurcation methods",

author = "D Rezgui and MH Lowenberg and PC Bunniss",

note = "Name and Venue of Event: Mini-Symposium 13: Flight Dynamics & Control Conference Organiser: The Chinese Society of Theoretical and Applied Mechanics (CSTAM)",

year = "2010",

month = may,

language = "English",

booktitle = "3rd International Conference on Dynamics, Vibration & Control, Hangzhou, China",

}

TY - GEN

T1 - Flap-lag stability of helicopter rotor blades using continuation and bifurcation methods

AU - Rezgui, D

AU - Lowenberg, MH

AU - Bunniss, PC

N1 - Name and Venue of Event: Mini-Symposium 13: Flight Dynamics & Control Conference Organiser: The Chinese Society of Theoretical and Applied Mechanics (CSTAM)

PY - 2010/5

Y1 - 2010/5

M3 - Conference Contribution (Conference Proceeding)

BT - 3rd International Conference on Dynamics, Vibration & Control, Hangzhou, China

ER -

Flap-lag stability of helicopter rotor blades using continuation and bifurcation methods

Bibliographical note

Handle.net

Activities

The 3rd International Conference on Dynamics, Vibration and Control (ICDVC)

Cite this