Tail Area Reduction for Aircraft with Spanwise Distributed Electric Propulsion
2018 AIAA/IEEE Electric Aircraft Technologies Symposium (EATS)（2018）
关键词
empennage design,vertical tail area,larger-than-nominal vertical tail,lighter weight microgrid architecture,differential thrust,active control,asymmetric thrust design condition,electric microgrid,driving requirements,electrically driven propulsors,spanwise arrays,spanwise distributed electric propulsion,aircraft,tail area reduction
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