Modeling and Simulation of a Parallel Hybrid Electric Regional Aircraft for the Electrified Powertrain Flight Demonstration (EPFD) Program

Author:

Cinar Gokcin1,Cai Yu2,Denney Russell K.2,Mavris Dimitri N.2

Affiliation:

1. University of Michigan,Department of Aerospace Engineering,Ann Arbor,Michigan,48109–2140

2. Institute of Technology,,School of Aerospace Engineering Georgia,Atlanta,Georgia,30332–0150

Publisher

IEEE

Reference17 articles.

1. Modeling turboshaft engines for the revolutionary vertical lift technology project;snyder;Vertical Flight Society 75th Annual Forum & Technology Display,2019

2. Component arrangement studies for an 8000 shp turboshaft high technology core

3. Next Generation 2 MW Turboshaft and Turboprop Engines

4. Algorithm for calculating turbine cooling flow and the resulting decrease inturbine efficiency;gauntner;National Aeronautics and Space Administration Tech Rep NASA/TM-81453,1980

5. Simultaneous multi-design point approach to gas turbine on-design cycle analysis for aircraft engines;schutte;Ph D Dissertation Georgia Institute of Technology,2009

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