CFD-Based Aeroelastic Sensitivity Study of a Low-Speed Flutter Demonstrator

Title:: CFD-Based Aeroelastic Sensitivity Study of a Low-Speed Flutter Demonstrator
Document type:: Zeitschriftenaufsatz
Author(s):: Rozov, Vladyslav; Volmering, Andreas; Hermanutz, Andreas; Hornung, Mirko; Breitsamter, Christian
Abstract:: The goal of developing aircraft that are greener, safer and cheaper can only be maintained through significant innovations in aircraft design. An integrated multidisciplinary design approach can lead to an increase in the performance of future derivative aircraft. Advanced aerodynamics and structural design technologies can be achieved by both passive and active suppression of aeroelastic instabilities.
Keywords:: Antisymmetric boundary condition; Computational aeroelasticity; FLEXOP; Flutter analysis; Flutter demonstrator; Linearized CFD; SD-CFD; Sensitivity study; Stability analysis
Journal title:: Aerospace
Year:: 2019
Journal volume:: 6
Journal issue:: 3
Pages contribution:: 30
Covered by:: Scopus
Fulltext / DOI:: doi:10.3390/aerospace6030030
WWW:: https://www.mdpi.com/2226-4310/6/3/30
Publisher:: MDPI AG
E-ISSN:: 2226-4310
Submitted:: 06.02.2019
Accepted:: 01.03.2019
Date of publication:: 06.03.2019
TUM Institution:: Lehrstuhl für Aerodynamik und Strömungsmechanik
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