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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