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Conceptual Design of a Single-Aisle Turboelectric Commercial Transport With Fuselage Boundary Layer Ingestion Overview
- Concept description
- Quick summary of results
- N+3 Conventional Configuration
- Description of baseline
- Comparison of baseline to Refined SUGAR concept
- Simplifying assumptions
- Propulsion system modeling
- Boundary layer modeling
- System performance
- Weight estimates
- System design space exploration
- Results
- Turboelectric concept benefits
- System sensitivities
- Future work
- Conclusions
Document ID
20200008565
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Jason R. Welstead (Langley Research Center Hampton, Virginia, United States)
James L. Felder (Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
May 18, 2020
Subject Category
Aeronautics (General)
Report/Patent Number
Report Number: NF1676L-23318
NF1676L-23318
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics Science and Technology Forum and Exposition 2016 (AIAA SciTech 2016)
Location: San Diego, CA
Country: US
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 081876.02.07.30.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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