Passive flutter suppression using a nonlinear tuned vibration absorber

التفاصيل البيبلوغرافية
العنوان: Passive flutter suppression using a nonlinear tuned vibration absorber
المؤلفون: Verstraelen, Edouard, Gourc, Etienne, Kerschen, Gaëtan, Dimitriadis, Grigorios
المصدر: NNM2016 Liège Conference, 4 Juillet 2016 au 8 Juillet 2016
سنة النشر: 2016
مصطلحات موضوعية: wind tunnel testing, nonlinear aeroelasticity, nonlinear tuned vibration absorber, bifurcation, Engineering, computing & technology, Aerospace & aeronautics engineering, Ingénierie, informatique & technologie, Ingénierie aérospatiale
الوصف: A recent study showed that the addition of a linear tuned vibration absorber could increase the flutter speed of a rigid wing with pitch and flap degrees of freedom by about 35%. However, the absorber was turning the initial super-critical bifurcation into a sub-critical one. This work shows numerically that adding a nonlinear restoring force to the absorber can restore the su- percritical behaviour of the bifurcation and further reduce the post-instability limit cycle amplitude.
The Nonlinear Tuned Vibration Absorber (NoVib)
نوع الوثيقة: conference poster not in proceedings
http://purl.org/coar/resource_type/c_18co
conferencePoster
وصف الملف: A0
اللغة: English
Relation: info:eu-repo/grantAgreement/EC/FP7/307265
URL الوصول: https://orbi.uliege.be/handle/2268/200224
حقوق: open access
http://purl.org/coar/access_right/c_abf2
info:eu-repo/semantics/openAccess
رقم الأكسشن: edsorb.200224
قاعدة البيانات: ORBi