Aerodynamic Conceptual Design of Boundary Layer Ingestion Propulsor Systems: Hybrid Wingbody Aircraft with Propulsion-Airframe-Integration
2018 Applied Aerodynamics Conference
01.01.2018
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Conceptual Analysis of Boundary Layer Ingestion towards Aircraft Propulsion Integration
British Library Conference Proceedings | 2013
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