Title: Aeroelastic analysis of turboprop commuter aircraft with tip-tanks
Authors: Čečrdle, J.
Vích, O.
Citation: Computational mechanics 2018: book of extended abstracts: 34th conference with international participation, p. 7-8.
Issue Date: 2018
Publisher: Západočeská univerzita v Plzni
Document type: konferenční příspěvek
URI: http://hdl.handle.net/11025/30781
ISBN: 978-80-261-0819-1
Keywords: aeroelastická analýza;turbovrtulové dopravní letadlo;křídlové nádrže
Keywords in different language: aeroelastic analysis;turboprop commuter aircraft;wing-tip tanks
Abstract in different language: This paper deals with aeroelastic (flutter) analysis of an aircraft with unconventional wing structure, which is specific by the installation of wing-tip tanks. The subjected aircraft is twin wing-mounted tractor turboprop commuter aircraft for 19 passengers, with a wingspan of 9.6 m and a maximal take-off weight of 7000 kg. The paper is focused on the assessment of specific flutter issue, originating from the unconventional wing configuration. Further, another flutter issues related to elevator flutter and rudder flutter are described.
Rights: Copyright © 2018 University of West Bohemia, Plzeň, Czech Republic
Appears in Collections:Computational mechanics 2018
Computational mechanics 2018

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