Designing and Testing a Blended Wing Body with Boundary-Layer Ingestion Nacelles
- 1 September 2006
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 43 (5), 1479-1489
- https://doi.org/10.2514/1.22765
Abstract
No abstract availableKeywords
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