Aero-propulsive Design Optimization of a Turboelectric Boundary Layer Ingestion Propulsion System
Author:
Affiliation:
1. NASA Glenn Research Center
2. NASA Ames Research Center
3. University of Michigan, Ann Arbor
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3976
Reference34 articles.
1. The Jet Airplane Utilizing Boundary Layer Air for Propulsion
2. Selection of a Propulsor for a Submersible System
3. Wake ingestion propulsion benefit
4. INTERFERENCE BETWEEN PROPELLER AND VEHICLE; THE DUCTED PROPELLER
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