This thesis presents two studies that illustrate how cost modelling can be integrated into the various design process stages, ranging from strategic gas turbine and airframe system design to preliminary and detailed component design and production planning. The first study investigates which cruise speed the next generation of short-haul aircraft with 150 seats should fly at and whether a conventional two- or three-shaft turbofan, a geared turbofan, a turboprop or an open rotor should be employed in order to make the aircraft's direct operating cost robust to uncertain fuel and carbon (CO2) prices in the Year 2030, taking the aircraft productivity, the passenger value of time and the modal shift into account. To answer this question, an opt...
Aero-engine customers today are demanding high quality, low cost products to meet their strict requi...
Aviation system planning, particularly fleet selection and adoption, is challenged by fuel price unc...
Central targets for jet engine research activities comprise the evaluation of improved engine compon...
This paper presents a study that numerically investigated which cruise speed the next generation of ...
This paper presents a project that is investigating which cruise speed the next generation of short-...
Turboprop aircraft achieve higher propulsive efficiencies at lower speeds due to their engine’s abil...
The gas turbine engine has evolved rapidly during past decades to provide a reliable and efficient b...
This paper carries out an optimization study for a conventional and a geared turbofan engine by mini...
This paper carries out an optimization study for a conventional and a geared turbofan engine by mini...
A major issue, which has prevented aircraft manufacturers from implementing efficient and cost-effec...
Aircraft design activities involve several disciplines, whose effects are typically interrelated wit...
One of the steps in the complex design of aircraft propulsion system consists of designing an effici...
In this multidisciplinary study a geared open rotor configuration is assessed and compared to an ult...
Conceptual and preliminary design phases of aerospace gas turbines compromise a particularly uncerta...
Introduction At GE Aircraft Engines (GEAE), during the preliminary design process for aircraft propu...
Aero-engine customers today are demanding high quality, low cost products to meet their strict requi...
Aviation system planning, particularly fleet selection and adoption, is challenged by fuel price unc...
Central targets for jet engine research activities comprise the evaluation of improved engine compon...
This paper presents a study that numerically investigated which cruise speed the next generation of ...
This paper presents a project that is investigating which cruise speed the next generation of short-...
Turboprop aircraft achieve higher propulsive efficiencies at lower speeds due to their engine’s abil...
The gas turbine engine has evolved rapidly during past decades to provide a reliable and efficient b...
This paper carries out an optimization study for a conventional and a geared turbofan engine by mini...
This paper carries out an optimization study for a conventional and a geared turbofan engine by mini...
A major issue, which has prevented aircraft manufacturers from implementing efficient and cost-effec...
Aircraft design activities involve several disciplines, whose effects are typically interrelated wit...
One of the steps in the complex design of aircraft propulsion system consists of designing an effici...
In this multidisciplinary study a geared open rotor configuration is assessed and compared to an ult...
Conceptual and preliminary design phases of aerospace gas turbines compromise a particularly uncerta...
Introduction At GE Aircraft Engines (GEAE), during the preliminary design process for aircraft propu...
Aero-engine customers today are demanding high quality, low cost products to meet their strict requi...
Aviation system planning, particularly fleet selection and adoption, is challenged by fuel price unc...
Central targets for jet engine research activities comprise the evaluation of improved engine compon...