25th Congress of International Council of the Aeronautical Sciences, 3 - 8 September 2006, Hamburg, Germany
Paper ICAS 2006-P2.5

A STUDY ON AERODYNAMIC DESIGN INTEGRATION OF THE SUPERCRITICAL WING AND REAR-MOUNTED ENGINE CONFIGURATION

Z. D. Wang, M. H. Zhang, J. H. Wang
THE FIRST AIRCRAFT INSTITUTE of AVIC 1, China

Keywords: Supercritical Wing,Nacelle,Design Integration

Study on the behavior of the aerodynamic interferences of rear-mounted engine to a supercritical wing and its impact on the aerodynamic characteristics.The configuration studied is a civil regional aircraft for featuring a supercritical wing and rear-mounted high by –pass ratio turbofan engine with separate flow nacelle closely downstream.

view full paper