# A model-based prognostics method for fatigue crack growth in fuselage panels

> Research article (Chinese Journal of Aeronautics, 2019) · cited 21× · AI/ML

**Wikidata**: [openalex:W2911101933](https://www.wikidata.org/wiki/openalex:W2911101933)  
**Source**: https://4ort.xyz/entity/a-model-based-prognostics-method-for-fatigue-crack-growth-in-fuselage-panels