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
▾
Department Control of Aeroelastic Systems
▾
Location & Arrival
Research & Transfer
Research & Transfer
▾
Research infrastructure
▾
Research topics
▾
Control Systems
▾
Control engineering modeling
▾
Projects
Latest
Latest
▾
Technical articles
▾
News
▾
Social Media
▾
Events
Multimedia
Multimedia
▾
Publications
▾
Videos
Careers & Education
Careers & Education
▾
Job vacancies
▾
Information for Students
>
Latest
>
Technical articles
>
>
Preliminary Aeroelastic Stability Assessment of High Aspect Ratio Wing Aircraft
>
Relative spanwise spar heights of the UPWing configuration in comparison to the VirEnfREI wing
Home
>
Latest
>
Technical articles
>
Preliminary Aeroelastic Stability Assessment of High Aspect Ratio Wing Aircraft
>
Relative spanwise spar heights of the UPWing configuration in comparison to the VirEnfREI wing
Relative spanwise spar heights of the UPWing configuration in comparison to the VirEnfREI wing
Relative spanwise spar heights of the UPWing configuration in comparison to the VirEnfREI wing
Credit:
DLR (CC BY-NC-ND 3.0)
