Aeropropulsive Interaction and Thermal System Integration within the ECO-150: A Turboelectric Distributed Propulsion Airliner with Conventional Electric Machines

Author:

Schiltgen Benjamin T.1,Freeman Jeffrey1

Affiliation:

1. Empirical Systems Aerospace, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Reference30 articles.

1. 1Empirical Systems Aerospace, Inc. "Integration of an Advanced Cryogenic Electric Propulsion System (ACEPS) to Aerodynamically Efficient Subsonic Transport Aircraft," NASA SBIR Phase I Final Report, Contract No. NNX09CC86P, 2009.

2. 2Empirical Systems Aerospace, Inc. "The Design and Integration of a Distributed Fan Propulsion System within a Split-Wing," NASA SBIR Phase I Final Report, Contract No. NNX10CC81P, 2010.

3. Benefits and Concerns of Hybrid Electric Distributed Propulsion with Conventional Electric Machines

4. 4Empirical Systems Aerospace, Inc. "Cryogenic and Non-Cryogenic Hybrid Electric Distributed Propulsion with Integration of Airframe and Thermal Systems to Analyze Technology Influence," NASA SBIR Phase I Final Report, Contract No. NNX15CD15P, 2015.

5. Integrated Aerodynamic Benefits of Distributed Propulsion

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