A copy of this work was available on the public web and has been preserved in the Wayback Machine. The capture dates from 2020; you can also visit the original URL.
The file type is
2018 AIAA Aerospace Sciences Meeting
Structural configuration analysis of two advanced aircraft concepts with distributed hybridelectric propulsion is presented. These concepts are characterized by multiple wing-mounted electric propulsors, which are powered by turbo-generators. Based on lessons learned from previous structural analysis of unconventional concepts, high-fidelity finite element models of the aircraft wing with embedded electric propulsors are developed. Although a hybrid-electric propulsion system has noise anddoi:10.2514/6.2018-1747 fatcat:z3smoxub3rf6nm4lq6mlwsdnx4