Preliminary sizing methodologies for regional aircraft with liquid hydrogen fuel and SOFC-GT-Battery hybrid-electric powertrains

Employing Liquid Hydrogen for Fuel Cell Heat Recovery in Aircraft

Passenger reasons for mobility transition from jet to train and turboprop

An Assessment of a Regional Turboprop Featuring Wingtip-Mounted Propellers: Design Integration Coupling Propeller-Wing Aerodynamics and Structural Wing Weight

Engine Health Monitoring Demonstrator based on GPA: A Gas Path Analysis GPA concept developed using the Gas turbine Simulation Program (GSP)

Design and numerical investigation of swirl recovery vanes for the Fokker 29 propeller

Engine simulation models for the cycles of BE1 and report on obtained performance data: Model development with the Gas turbine Simulation Program (GSP)