1. Benefits of Parallel Hybrid Electric Propulsion for Aircraft and Rotorcraft Open Access Author: Decerio, Dalton Title: Benefits of Parallel Hybrid Electric Propulsion for Aircraft and Rotorcraft Graduate Program: Aerospace Engineering (MS) Keywords: hybridelectricaircraftrotorcraftconceptual designoptimizationpropulsion File: Download Decerio_Thesis_Final.pdf Committee Members: Amy Pritchett, Program Head/ChairDavid K Hall, Thesis Advisor/Co-AdvisorKaren Ann Thole, Committee MemberEdward Smith, Committee Member