Static and Fatigue Failure of Bolted Joints in Hybrid Composite-Aluminium Aircraft Structures.
Saved in:
Superior document: | Linköping Studies in Science and Technology. Dissertations Series ; v.1706 |
---|---|
: | |
Place / Publishing House: | Linköping : : Linkopings Universitet,, 2015. {copy}2015. |
Year of Publication: | 2015 |
Edition: | 1st ed. |
Language: | English |
Series: | Linköping Studies in Science and Technology. Dissertations Series
|
Online Access: | |
Physical Description: | 1 online resource (69 pages) |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Strength Analysis and Modeling of Hybrid Composite-Aluminum Aircraft Structures.
by: Kapidzic, Zlatan.
Published: (2013.) -
Experiments and Modelling of Composite-Aluminium Bolted Joints.
by: Wemming, Hannes.
Published: (2022.) - Fatigue of aircraft structures.
-
Modeling damage, fatigue and failure of composite materials / / edited by Ramesh Talreja and Janis Varna ; contributors A. Barroso [and twenty three others].
Published: (2016.) -
Composite materials for aircraft structures / [edited by] Alan Baker, Stuart Dutton, Donald Kelly.
Published: (c2004.)