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Certification
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keywords:(Certification)
Widespread Fatigue Damage - an issue for aging and new aircraft
Visual Environment for Structural Loads Computations for Stress Analysis of Aeronautical Structures
Validation procedure for nonlinear analysis of stringer stiffened CFRP panels
Validation of damage modelling in composite fuselage structures under high velocity impact
Validation of damage modelling in composite fuselage structures under high velocity impact
Transverse-weld tensile properties of a new Al-4Cu-2Si alloy as filler metal
The promised future of multi-core processors in avionics systems
The promised future of multi-core processors in avionics systems
The Analysis on the Effect of Ground Reflection in the Noise Test of Aircraft Engine
Technology selection for holistic analysis of hybrid-electric commuter aircraft
Submarine certification test using fiber optic sensors
Structural design and test capability of a CFRP aileron
Smoke Detectors interfaced by a safety critical aircraft based CAN-Bus Network
Review of Formal Agile Methods as Cost-Effective Airworthiness Certification Processes
Qualification of Avionic Software Based on Machine Learning: Challenges and Key Enabling Domains
Pseudo Fatigue Testing for Rapid Certification to Service
Progress in the airworthiness technology of civil aero-engine
Progress in the airworthiness technology of civil aero-engine
On the impact of deferred repair on the expected number of system failures - A stochastic model
On the certification of bonded composite repairs to primary aircraft structure
On-road optical remote sensing measurements of in-use bus emissions
Numerical investigation on carbon foam-based dampers for helicopter seats
Modelling Aerodynamics Unsteady Loads on the Horizontal Tail Plane of a Civil Aircraft
Laminated Windshield Breakage Modelling in the Context of Headform Impact Homologation Tests
Innovative, low-cost manufacturing of a wing-box section
Inference of torque and power from heavy-duty diesel engines for on-road emissions monitoring
High speed train aeroacoustic solution for community noise using lattice Boltzmann Method
Fuselage disbond inspection procedure using pulsed thermography
Fuel mass estimation in aircraft tanks using neural nets
From Design to Implementation: An Automated, Credible Autocoding Chain for Control Systems
Fire suppression in aircraft by solid propellant gas generators
Fire behaviour of carbon fibre epoxy composite for aircraft: Novel test bench and experimental study
Evaluation of the Testing Capabilities of the Q10 Prototype Dummy
Dynamic Damage of Aircraft Wing Leading Edge Impacted by Birds
Development of rigid-body HEV model for HILS certification test method
Development of Materials Characterization Procedure for Composite Aircraft
Development of a Language Model for Named-Entity-Recognition in Aerospace Requirements