Catherine Jones
strath.elsevierpure.com
0000-0001-7524-5756
University of Strathclyde
42 papers found
Refreshing results…
Sizing of Superconducting Cables for Turbo-ElectricDistributed Propulsion Aircraft Using a Particle Swarm Optimization Approach
Design of modular, CFRP-encased electrical power systems for more-electric aircraft applications
At scale, experimental capture of electrical response of carbon fibre composites to inform integrated electrical power and structural systems
A framework for efficient design of multifunctional-CFRP for future aircraft
A Modelling Design Framework for Integrated Electrical Power and Non-Electrical Systems Design on Electrical Propulsion Aircraft
Electrical protection solutions enabling integrated electrical power and composite structure systems for aircraft
A Route to Sustainable Aviation: A Roadmap for the Realization of Aircraft Components With Electrical and Structural Multifunctionality
A Modelling Framework for Efficient Design of Electrical Power Systems for Electrical Propulsion Aircraft
Voltage Based Current Compensation Converter Control for Power Electronic Interfaced Distribution Networks in Future Aircraft
First-Fault Detection in DC Distribution with IT Grounding based on Sliding Discrete Fourier-Transform
Protection and Fault Management Strategy Maps for Future Electrical Propulsion Aircraft
Grounding Topologies for Resilient, Integrated Composite Electrical Power Systems for Future Aircraft Applications
A Fault Management-Oriented Early-Design Framework for Electrical Propulsion Aircraft
A Novel Methodology for Macroscale, Thermal Characterization of Carbon Fiber-Reinforced Polymer for Integrated Aircraft Electrical Power Systems
Control of DC power distribution system of a hybrid electric aircraft with inherent overcurrent protection
Adaptive V/f-Based Control for Induction Machines in Distributed Electric Propulsion Systems
Electrical and Thermal Effects of Fault Currents in Aircraft Electrical Power Systems With Composite Aerostructures
Protection Requirements Capture for Superconducting Cables in TeDP Aircraft Using a Thermal-Electrical Cable Model
Establishing viable fault management strategies for distributed electrical propulsion aircraft
Impact of Key Design Constraints on Fault Management Strategies for Distributed Electrical Propulsion Aircraft
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