Modeling Boundary Layer Ingestion Using a Coupled Aeropropulsive Analysis
Author:
Affiliation:
1. NASA Glenn Research Center, Cleveland, Ohio 44139
2. University of Michigan, Ann Arbor, Michigan 48109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034601
Reference37 articles.
1. Selection of a Propulsor for a Submersible System
2. Conceptual Design of a Single-Aisle Turboelectric Commercial Transport with Fuselage Boundary Layer Ingestion
3. Turboelectric Distributed Propulsion Engine Cycle Analysis for Hybrid-Wing-Body Aircraft
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