An Alternative Configuration for Distributed Propulsion with Boundary Layer Ingestion on a Hybrid Wing Body Airframe
International symposium; 21st, Air breathing engines ; 2013 ; Busan, Korea
2013-01-01
7 pages
Includes bibliographical references and index
Conference paper
English
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Propulsion Airframe Aeroacoustic Integration Effects for a Hybrid Wing Body Aircraft Configuration
British Library Conference Proceedings | 2010
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