15 - Guest lectures
REASSESSMENT OF PARAMETRIC OPTIMIZATION AND PERFORMANCE ANALYSIS METHODOLOGY FOR MILD HYBRID AIRCRAFT PROPULSION SYSTEMS
J. Gladin¹, E. Aydin¹, J. Kenny¹, A. Burell¹, J. Decroix¹, T. Zaidi¹, R. Gautier¹, D. Mavris¹; ¹ASDL, United States
The refinement of a previously-published novel parametric framework for analyzing and optimizing hybrid electric propulsion systems is presented here. A study is performed using this framework, employing Boeing 737MAX with CFM LEAP-1B vehicle and engine model as the technology reference aircraft, and a mild hybrid turbofan and open rotor engine and mild hybrid open rotor modeled as well.