COMPARATIVE EFFICIENCY ANALYSIS OF DISTRIBUTED PROPULSION SYSTEMS FOR PROPULSIVE FUSELAGE AND HYBRID WING BODY CONCEPTS IN FP7 PROJECT “DISPURSAL”

摘要

The paper discusses results of investigation and analysis of advanced aircraft and propulsion system concepts with distributed propulsion, i.e. unconventional aircraft like Hybrid Wing Body with multiple fans driving by engine cores, as well as aircraft with an auxiliary single fan driven by an engine core installed in the fuselage aft cone (so called propulsive fuselage aircraft concept).