- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Event
-
Veröffentlichung
- (where)
-
Bonn
- (who)
-
Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.
- (when)
-
2021
- Creator
-
Nguyen-Hoang, M.
Becker, W.
- DOI
-
10.25967/490004
- URN
-
urn:nbn:de:101:1-2021020513044383016605
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
25.03.2025, 1:49 PM CET
Data provider
This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Nguyen-Hoang, M.
- Becker, W.
- Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.
Time of origin
- 2021
Other Objects (12)
Mechanism Based Constitutive Model for Composite Laminates
Dimensioning of Punctiform Metal-Composite Joints: A Section-Force Related Failure Criterion : Dimensioning of Punctiform Metal-Composite Joints: A Section-ForceRelated Failure Criterion
A Numerical Failure Analysis of Multi-bolted Joints in FRP Laminates Based on Basalt Fibers☆
Static aerolastic optimization of composite wings with variable stiffness laminates
Preliminary design of composite joints : [bonded joints ; bolted joints ; loops]
Variable mixed mode fatigue delamination in composite laminates : testing and analysis
Sensitivity analysis of interface fatigue crack propagation in elastic composite laminates
Sensitivity analysis of interface fatigue crack propagation in elastic composite laminates
Modeling of ultrasonic wave propagation in composite laminates with realistic discontinuity representation
Test Setup for Investigating the Impact Behavior of Biaxially Prestressed Composite Laminates
Adaptive, tolerant and efficient composite structures
Identification of failure mechanisms in CFRP laminates using 3D digital image correlation
Mechanism Based Constitutive Model for Composite Laminates
Dimensioning of Punctiform Metal-Composite Joints: A Section-Force Related Failure Criterion : Dimensioning of Punctiform Metal-Composite Joints: A Section-ForceRelated Failure Criterion
A Numerical Failure Analysis of Multi-bolted Joints in FRP Laminates Based on Basalt Fibers☆
Static aerolastic optimization of composite wings with variable stiffness laminates
Preliminary design of composite joints : [bonded joints ; bolted joints ; loops]
Variable mixed mode fatigue delamination in composite laminates : testing and analysis
Sensitivity analysis of interface fatigue crack propagation in elastic composite laminates
Sensitivity analysis of interface fatigue crack propagation in elastic composite laminates
Modeling of ultrasonic wave propagation in composite laminates with realistic discontinuity representation
Test Setup for Investigating the Impact Behavior of Biaxially Prestressed Composite Laminates
Adaptive, tolerant and efficient composite structures
Identification of failure mechanisms in CFRP laminates using 3D digital image correlation
Mechanism Based Constitutive Model for Composite Laminates
Dimensioning of Punctiform Metal-Composite Joints: A Section-Force Related Failure Criterion : Dimensioning of Punctiform Metal-Composite Joints: A Section-ForceRelated Failure Criterion
A Numerical Failure Analysis of Multi-bolted Joints in FRP Laminates Based on Basalt Fibers☆
Static aerolastic optimization of composite wings with variable stiffness laminates
Preliminary design of composite joints : [bonded joints ; bolted joints ; loops]
Variable mixed mode fatigue delamination in composite laminates : testing and analysis
Sensitivity analysis of interface fatigue crack propagation in elastic composite laminates
Sensitivity analysis of interface fatigue crack propagation in elastic composite laminates
Modeling of ultrasonic wave propagation in composite laminates with realistic discontinuity representation
Test Setup for Investigating the Impact Behavior of Biaxially Prestressed Composite Laminates
Adaptive, tolerant and efficient composite structures