Skip to main content
Skip to navigation
Skip to footer
DLR Portal
Press
Accessibility
de
en
Institute of Aeroelasticity
About us
About us
▾
The Institute of Aeroelasticity
▾
Departments
▾
Department Aeroelastic Experiments
▾
Department Aeroelastic Simulation
▾
Department Loads Analysis and Design
▾
Department Structural Dynamics and System Identification
▾
Location & Arrival
Research & Transfer
Research & Transfer
▾
Research infrastructure
▾
High pressure wind tunnel Göttingen
▾
Multi axis vibration simulator (MAVIS)
▾
The Non-Rotating Annular Test Facility
▾
Measurement Technology and Test Rigs
▾
Research topics
▾
Aeroelastic Design
▾
Aeroelasticity of Turbomachinery
▾
Aeroelastic Simulation of Wind Turbines
▾
Aeroelastic Stability and System Response
▾
Aeroelastic System Identification
▾
Aeroelastic Wind Tunnel Experiments
▾
Loads Analysis
▾
Measurement and Testing Technology
▾
Structural Dynamic Experiments
▾
Unsteady Aerodynamics
▾
Vibroacoustics
Latest
Latest
▾
Technical articles
▾
News
▾
Social Media
Mulitmedia
Mulitmedia
▾
Publications
▾
Videos
Careers & Education
Careers & Education
▾
Job vacancies
▾
Information for Students
>
Latest
>
Technical articles
>
Technical article 2022
>
>
Semi-active flutter suppression
>
Changes in the flutter stability boundary in the transonic flow regime due to a spoiler deflection
Home
>
Latest
>
Technical articles
>
Technical article 2022
>
Semi-active flutter suppression
>
Changes in the flutter stability boundary in the transonic flow regime due to a spoiler deflection
Changes in the flutter stability boundary in the transonic flow regime due to a spoiler deflection
Changes in the flutter stability boundary in the transonic flow regime due to a spoiler deflection
Credit:
DLR (CC BY-NC-ND 3.0)
