Skip to main content
Skip to navigation
Skip to footer
DLR Portal
Press
Accessibility
de
en
Institute of
Structures and Design
About us
About us
▾
The Institute of Structures and Design
▾
Departments
▾
Automation and Quality Assurance in Production Technology
▾
Component Design and Manufacturing Technologies
▾
Ceramic Composites and Structures
▾
Structural Integrity
▾
Space System Integration
▾
Locations & Arrival
▾
Stuttgart
▾
Augsburg
Research & Transfer
Research & Transfer
▾
Research Topics
▾
High-Performance Lightweight Structures
▾
CMC Technology and Structures
▾
Lightweight Structures for Space Applications
▾
Aero Engine Structures
▾
Projects
▾
Ongoing projects
▾
Project archive
▾
Research infrastructure
▾
Start-Ups
Latest
Latest
▾
News
▾
Events
▾
Press review
Multimedia
Multimedia
▾
Publications
▾
Videos
Careers & Education
Careers & Education
▾
Job vacancies at the institute
▾
Information for students
>
Research & Transfer
>
Projects
>
Project archive
>
>
Project CREVAD – Crash evaluation of alternative CFRP fuselage designs
>
Kinematics of a crash conept using tension loads for energy absorption
Home
>
Research & Transfer
>
Projects
>
Project archive
>
Project CREVAD – Crash evaluation of alternative CFRP fuselage designs
>
Kinematics of a crash conept using tension loads for energy absorption
Kinematics of a crash conept using tension loads for energy absorption
Kinematics of a crash conept using tension loads for energy absorption
Credit:
© DLR. All rights reserved
