When looking into aircraft hybrid electric propulsion development, a combination of disciplines and expertise is needed to achieve the required performance.
Based on the model-based systems engineering (MBSE) approach, designers can assess hybrid electric configurations, with respect to engine operability, thermal management and overall integrated performance.
In this webinar, we highlight two cases. The first one is related to the hybridization of an existing regional aircraft, the ATR 42-500. The second one will feature the mission analysis of complete rotorcraft operations.
Business Development Manager, Simcenter System Simulation solutions for Aerospace