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What is Nacelle-Airframe Integration for BWB Design about?

This paper presents a nacelle-airframe integration design method for blended-wing-body (BWB) transport aircraft with podded engines, addressing issues of strong shock waves and flow separation. The proposed method utilizes numerical simulations to optimize the design by channeling airflow and reducing drag, achieving an 8.7% reduction in cruise drag despite an increase in nacelle pressure drag. The study emphasizes the importance of contouring and positioning of nacelles to enhance aerodynamic performance a

Author

Emircan Balık

Language

EN