Paper
23 November 2022 Effect study of Nacelle’s installation angles for blended-wing-body aircraft
Liu Yang, Yuan Zhong, Kaili Liu, Xinyu Yang
Author Affiliations +
Proceedings Volume 12302, Seventh International Conference on Electromechanical Control Technology and Transportation (ICECTT 2022); 123021Z (2022) https://doi.org/10.1117/12.2645332
Event: Seventh International Conference on Electromechanical Control Technology and Transportation (ICECTT 2022), 2022, Guangzhou, China
Abstract
Blended-Wing-Body (BWB) is a special aircraft design concept which combines the fuselage and wing together. The unique shape of blended-wing-body aircraft owns the advantages of high pneumatic efficiency, light structural weight and large capacity. Blended-wing-body not only saves energy and environmental protection, but also effectively reduces noise and harmful gas emission of the engine. In this paper, the effect of blended-wing-body nacelle’s installation angle of title and toe of the aircraft is studied by optimizing and analyzing. The changes of detachment area of flow on the surface of fuselage and nacelle are mainly researched. The nacelle’s installation angle of title and toe is proved to influence the elimination of flow detachment exactly.
© (2022) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Liu Yang, Yuan Zhong, Kaili Liu, and Xinyu Yang "Effect study of Nacelle’s installation angles for blended-wing-body aircraft", Proc. SPIE 12302, Seventh International Conference on Electromechanical Control Technology and Transportation (ICECTT 2022), 123021Z (23 November 2022); https://doi.org/10.1117/12.2645332
Advertisement
Advertisement
RIGHTS & PERMISSIONS
Get copyright permission  Get copyright permission on Copyright Marketplace
KEYWORDS
Analytical research

Aerodynamics

CFD analysis

Numerical simulations

Back to Top