Experimental Validation of a Computational Hybrid Methodology to Estimate Fuselage Damage Due to Harsh Landing
2016
Article (Journal)
English
Helicopter Harsh Landing Events: A Computational Hybrid Methodology to Estimate Fuselage Damage
Online Contents | 2013
|Model-Based Structural Integrity Assessment of Helicopter Fuselage During Harsh Landing
British Library Conference Proceedings | 2015
|Model-Based Structural Integrity Assessment of Helicopter Fuselage During Harsh Landing
British Library Conference Proceedings | 2015
|Harsh Landing Ultimate Sensor Fusion
IEEE | 2024
|