Flutter and Limit Cycle Oscillation Suppression Using Linear and Nonlinear Tuned Vibration Absorbers

Autor:	Grigorios Dimitriadis, Gaëtan Kerschen, Edouard Verstraelen
Rok vydání:	2017
Předmět:	Physics 02 engineering and technology 021001 nanoscience & nanotechnology Aeroelasticity 01 natural sciences Moving shock 010305 fluids & plasmas Vibration Nonlinear system Dynamic Vibration Absorber Control theory 0103 physical sciences Flutter 0210 nano-technology Transonic Bifurcation
Zdroj:	Shock & Vibration, Aircraft/Aerospace, Energy Harvesting, Acoustics & Optics, Volume 9 ISBN: 9783319547343
DOI:	10.1007/978-3-319-54735-0_32
Popis:	Aircraft are more than ever pushed to their limits for performance reasons. Consequently, they become increasingly nonlinear and they are more prone to undergo aeroelastic limit cycle oscillations. Structural nonlinearities affect aircraft such as the F-16, which can undergo store-induced limit cycle oscillations (LCOs). Furthermore, transonic buzz can lead to LCOs because of moving shock waves in transonic flight conditions on many aircraft.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::033da1c5cc9a5f7840129625761b1e1f https://doi.org/10.1007/978-3-319-54735-0_32 Zobrazit plný text záznamu