Numerical simulations of transonic flutter on a three-dimensional wing

Ritsuya Hoshi, Yuichi Kuya, Keisuke Sawada

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Fluid-structure interaction analysis is carried out to find the transonic flutter boundary for a realistic high aspect-ratio main wing of a typical medium-sized civil transport aircraft having supercritical wing section and twist distribution. We consider two cases in which the interaction analysis starts either from the static aeroelastic equilibrium shape or from the jig shape. It is found that both cases could determine the transonic dip of the flutter boundary equally well. However, the case of starting from the jig shape is shown to determine the flutter boundary substantially faster than the case of starting from aeroelastic equilibrium shape.

Original languageEnglish
Title of host publicationAIAA Scitech 2020 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
Pages1-15
Number of pages15
ISBN (Print)9781624105951
DOIs
Publication statusPublished - 2020
EventAIAA Scitech Forum, 2020 - Orlando, United States
Duration: 2020 Jan 62020 Jan 10

Publication series

NameAIAA Scitech 2020 Forum

Conference

ConferenceAIAA Scitech Forum, 2020
CountryUnited States
CityOrlando
Period20/1/620/1/10

ASJC Scopus subject areas

  • Aerospace Engineering

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