Conceptual Design of Distributed Electrified Boundary Layer Ingesting Propulsors for the CHEETA Aircraft Concept
Author:
Affiliation:
1. Massachusetts Institute of Technology
2. Pennsylvania Institute of Technology
3. University of Illinois, Urbana-Champaign
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-3287
Reference27 articles.
1. Electrified Aircraft Trade-Space Exploration
2. A Review of Distributed Electric Propulsion Concepts for Air Vehicle Technology
3. Mission Analysis and Emissions for Conventional and Hybrid-Electric Commercial Transport Aircraft
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