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2. Benefits of Parallel Hybrid Electric Propulsion for Aircraft and Rotorcraft

open_access
Open Access
Author:
Decerio, Dalton
Title:
Benefits of Parallel Hybrid Electric Propulsion for Aircraft and Rotorcraft
Graduate Program:
Aerospace Engineering (MS)
Keywords:
hybrid
electric
aircraft
rotorcraft
conceptual design
optimization
propulsion
File:
Download Decerio_Thesis_Final.pdf
Committee Members:
Amy Pritchett, Program Head/Chair
David K Hall, Thesis Advisor/Co-Advisor
Karen Ann Thole, Committee Member
Edward Smith, Committee Member