The concept of distributed propulsion is to integrate the propulsion system with the airframe to exploit synergies of such a configuration. This report describes a CFD study of the aerodynamic effect of distributed propulsion. Firstly, a preliminary design model is established and studied. Several configurations of 2D model of distributed propulsion have been analyzed, using a new BC to model the engine. Finally a 3D model of an aircraft equipped with a distributed system is studied
Numerical investigation of aerodynamic effects of distributed propulsion
Toniato, Pierpaolo
2014/2015
Abstract
The concept of distributed propulsion is to integrate the propulsion system with the airframe to exploit synergies of such a configuration. This report describes a CFD study of the aerodynamic effect of distributed propulsion. Firstly, a preliminary design model is established and studied. Several configurations of 2D model of distributed propulsion have been analyzed, using a new BC to model the engine. Finally a 3D model of an aircraft equipped with a distributed system is studiedFile in questo prodotto:
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Utilizza questo identificativo per citare o creare un link a questo documento:
https://hdl.handle.net/20.500.12608/17924