Design of Airframe-Integrated, Distortion-Tolerant Propulsion Systems
2011
14 pages
Report
Keine Angabe
Englisch
Aircraft , Test Facilities & Equipment , Propulsion system configurations , Engine design , Engine airframe integration , Engine inlets , Distortion , Computational fluid dynamics , Blended-wing-body configurations , Boeing aircraft , Propulsive efficiency , Boundary layers , Optimization , Fan blades , Shape optimization
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