Show simple item record

dc.contributor.authorOzcatalbas, M.
dc.contributor.authorAcar, B.
dc.contributor.authorUslu, Sıtkı
dc.date.accessioned2021-01-27T13:45:03Z
dc.date.available2021-01-27T13:45:03Z
dc.date.issued2020-06
dc.identifier.citationOzcatalbas, M., Acar, B., and Uslu, S. (2020). Effect of Free-Play and Initial Conditions on Aeroelastic Behavior of a Missile Canard in Supersonic Flow. In AIAA AVIATION 2020 FORUM (p. 2663).en_US
dc.identifier.isbn978-162410598-2
dc.identifier.urihttps://arc.aiaa.org/doi/10.2514/6.2020-2663
dc.identifier.urihttp://hdl.handle.net/20.500.11851/4121
dc.descriptionAIAA AVIATION 2020 FORUM (2020 : Virtual, Online)en_US
dc.description.abstractCanards are used as control surfaces and they operate with control systems including actuators, drivelines and electronics in missiles. Aeroelastic behavior of the canards must be accurately known to comply with the control systems. However, structural nonlinearities such as plastic deformation, bilinear stiffness and free-play change the aeroelastic characteristics of the structure. This study aims to illustrate nonlinear aeroelastic behavior of a missile canard which has free-play in its shaft-actuator joint. Three initial angle of attack positions and two different free-play sizes were evaluated with fluid-structure interaction (FSI) method. Nonlinear behavior of the canard was compared with the linear, which has no free-play, condition. Consequently, FSI results showed that response frequencies decrease as free-play increases and amplitudes of oscillations are affected by initial conditions. © 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.en_US
dc.language.isoengen_US
dc.publisherAmerican Institute of Aeronautics and Astronautics Inc, AIAAen_US
dc.relation.ispartofAIAA AVIATION 2020 FORUM
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectFlutter en_US
dc.subject Gust Loads en_US
dc.subject Unsteady Aerodynamicsen_US
dc.titleEffect of free-play and initial conditions on aeroelastic behavior of a missile canard in supersonic flowen_US
dc.typeconferenceObjecten_US
dc.contributor.departmentTOBB ETU, Faculty of Engineering, Department of Mechanical Engineeringen_US
dc.contributor.departmentTOBB ETÜ, Mühendislik Fakültesi, Makine Mühendisliği Bölümütr_TR
dc.identifier.scopus2-s2.0-85092512642
dc.contributor.tobbetuauthorUslu, Sıtkı
dc.contributor.YOKid143686
dc.identifier.doi10.2514/6.2020-2663
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıtr_TR


Files in this item

FilesSizeFormatView

There are no files associated with this item.

This item appears in the following Collection(s)

Show simple item record