479.575 PEOPLE
| People | Locations | Statistics |
|---|---|---|
| Ziakopoulos, Apostolos | Athens |
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| Vigliani, Alessandro | Turin |
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| Catani, Jacopo | Rome |
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| Statheros, Thomas | Stevenage |
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| Utriainen, Roni | Tampere |
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| Guglieri, Giorgio | Turin |
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| Martínez Sánchez, Joaquín |
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| Tobolar, Jakub |
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| Volodarets, M. |
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| Piwowar, Piotr |
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| Tennoy, Aud | Oslo |
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| Matos, Ana Rita |
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| Cicevic, Svetlana |
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| Sommer, Carsten | Kassel |
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| Liu, Meiqi |
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| Pirdavani, Ali | Hasselt |
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| Niklaß, Malte |
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| Lima, Pedro | Braga |
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| Turunen, Anu W. |
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| Antunes, Carlos Henggeler |
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| Krasnov, Oleg A. |
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| Lopes, Joao P. |
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| Turan, Osman |
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| Lučanin, Vojkan | Belgrade |
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| Tanaskovic, Jovan |
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Giglio, Marco
Politecnico di Milano
in Cooperation with on an Cooperation-Score of 37%
Topics
- aircraft
- pylon
- modeling
- helicopter
- qualification
- fatigue cracking
- structural health monitoring system
- assessment
- estimate
- landing
- chemical element
- behavior
- maintenance
- monitoring
- validation
- altitude
- synthetic
- system safety
- fuselage
- duct
- rotor
- algorithm
- velocity
- neural network
- sensor
- face
- filtration
- strain gage
- bird
- bird strike
- honeycomb structure
- impact test
- health
- structural health monitoring
- simulation
- hub
- cracking
- composite material
- failure analysis
- protection
- drive shaft
- aluminum
- optimisation
- driving
- flight
- electromagnetic spectrum
- data
- estimating
- diagnosis
- alarm system
- strain measurement
- titanium
- numerical analysis
- graphite
- filament
- fatigue strength
- alloy
- peening
- residual stress
- emergency
- engineering
- fire
- library
- wire
- fatigue test
- bending
- hoist
- wire rope
- show 38 more
Publications (34/34 displayed)
- 2019Investigation about the structural nonlinearities of an aircraft pyloncitations
- 2017Analysis of a helicopter main gearbox by means of numerical modelling approach
- 2016Model-Assisted performance qualification of a distributed SHM system for fatigue crack detection on a helicopter tail boom
- 2016Experimental validation of a computational hybrid methodology to estimate fuselage damage due to harsh landingcitations
- 2015Model-based structural integrity assessment of helicopter fuselage during harsh landing
- 2015Experimental and numerical evaluation of the residual structural integrity of a helicopter tail rotor shaft subjected to ballistic impact
- 2015Low-velocity impact monitoring system for a helicopter frame by means of an artificial neural network
- 2013MEMS for structural health monitoring in aircraftcitations
- 2013Helicopter harsh landing events: A computational hybrid methodology to estimate fuselage damagecitations
- 2013Artificial neural networks for structural health monitoring of helicopter harsh landingscitations
- 2012Numerical simulation of the slant fracture of a helicopter's rotor hub with ductile damage failure criteriacitations
- 2012Diagnostic system validation for damage monitoring of helicopter fuselage
- 2012ANN based Bayesian hierarchical model for crack detection and localization over helicopter fuselage panels
- 2011Terminal ballistic effect on the crack growth assessment of a helicopter rotor drivecitations
- 2011Investigation on the fatigue life of an Al 8090 helicopter riveted t-jointcitations
- 2011Failure analysis of a composite main rotor helicopter hubcitations
- 2011Protection effect on a ballistic impact of NATO 7.62 ball bullet into helicopter drive shaft: Numerical simulationcitations
- 2011Sensor network optimization for damage detection on aluminium stiffened helicopter panels
- 2011Corrigendum to ''Defect tolerance assessment of a helicopter component subjected to multiaxial load'' [Eng. Fract. Mech. 77 (2010) 2479-2490]
- 2010Effect of cold driving process on fatigue life of helicopter fuselage joints
- 2010Effect of flight spectrum loads on the damage tolerance evaluation of a helicopter framecitations
- 2010Ballistic impact on a transmission tail rotor shaft for helicopter
- 2010Comparison of fatigue crack propagation behavior of Al 2024 and Al-Li 8090 helicopter fuselage panelscitations
- 2010Defect tolerance assessment of a helicopter component subjected to multiaxial loadcitations
- 2010Probability of detection and false alarms for metallic aerospace panel health monitoring
- 2009Helicopter fuselage crack monitoring and prognosis through on-board sensor network
- 2009Experimental and numerical investigation on fatigue failure of composite helicopter Main Rotor Hub
- 2009Effect of shot peening residual stresses on fatigue strength and crack propagation threshold: experience on helicopter components made in Al 7475 alloy
- 2008Crack propagation on helicopter panel: Experimental test and analysiscitations
- 20073D fatigue crack propagation analysis of a helicopter component
- 2007Fatigue life analysis of Al 8090 helicopter fuselage panels
- 2007TSA-FEM comparative analysis of a helicopter component under multiaxial load
- 2007Determination of the fatigue life of a helicopter tail rotor transmission subjected to ballistic damagecitations
- 2003Bending fatigue tests on a metallic wire rope for aircraft rescue hoistscitations
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