DLR Portal
Home
|
Sitemap
|
Contact
Imprint and terms of use
Privacy
Cookies & Tracking
|
Deutsch
You are here:
Home
:
Institute
:
Facilities
Advanced Search
News
Trade Fairs and Events
Institute
Mission Statement
Cooperations and Networks
Quality Management
Facilities
Staff
How to find us
Departments
Wissenswelt Leichtbau
Center for Lightweight-Production-Technology
Business Areas
Strategic Fields
Projects
Publications and Media Library
Curriculum
Jobs
Test Equipment
Back
Print
Interlaminar Composite Parameter Identification
Omega-Stringer Pull-Off Test Rig
Test rig for investigating the bonding strength at the interface between Omega-Stringer and skin
Comparison of different Omega-Stringer-geometries and bonding technics
Stringer pull-off test rig with Omega-stringer
Max. load
+/- 10 kN
Angle of load application
+/- 45° in 5° increments
Pitch of 2-point support
40 … 240 mm
Width of test specimen
100 mm
Stringer geometry
Omega, different on request
Clamping
2-point or 3-point
3D-Biax Test Rig
Test rig for investigating the interlaminar strength of thick laminas under tension, compression or shear load and the combination of these loadings
continuously adjusting between compression and shear or tension and shear
Determination of material properties in thickness direction
3D-Biax test rig with tension-shear specimen (in thickness direction)
Max. load
100 kN
Cross section of specimen
10 mm x 10 mm
Combined loading
Tension, compression, shear, tension-shear, compression-shear
Copyright © 2024 German Aerospace Center (DLR). All rights reserved.