Experimental identification of an aircraft piccolo tube exhibiting nonsmooth nonlinearities

T. Dossogne, M. Schoukens, B. Bernay, J.M.M.G. Noël, G. Kerschen

Onderzoeksoutput: Hoofdstuk in Boek/Rapport/CongresprocedureConferentiebijdrageAcademic


Piccolo tubes are parts of aircraft wings anti-icing system and consist of titanium pipes inserted into the internal structure of the slat. Due to thermal expansion, clearances between the tube and its support are unavoidable, and cause the overall system to exhibit highly nonlinear behaviour, resulting from impacts and friction. This paper aims the complete nonlinear vibration analysis of an aircraft Piccolo tube, from measurements and identification to a thorough understanding of the dynamics and improvements of the
Originele taal-2Engels
TitelProceedings of the 9th European Nonlinear Oscillations Conference (ENOC)
RedacteurenG. Stépán, G. Csernák
Plaats van productieBudapest
Aantal pagina's2
StatusGepubliceerd - jun 2017
Extern gepubliceerdJa
Evenement9th European Nonlinear Oscillations Conference (ENOC 2017) - Budapest University of Technology and Economics, Budapest, Hongarije
Duur: 25 jun 201730 jun 2017
Congresnummer: 9


Congres9th European Nonlinear Oscillations Conference (ENOC 2017)
Verkorte titelENOC 2017
Internet adres


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