e170226aFinal00091 The Effect of Adhesively Bonded Doubler Repairs on Existing Fatigue Cracks in Typical Combat Aircraft Structures
2018
Conference paper
English
BKL: | 55.50 Luftfahrzeugtechnik |
Towards a Certification Methodology for Adhesively Bonded Structures and Repairs
British Library Conference Proceedings | 1999
|Interfacial cracks in adhesively bonded scarf joints
AIAA | 1981
|Fatigue Damage Prediction for Bonded Composite Repairs Applied to Metallic Aircraft Structures
SAE Technical Papers | 2001
|