02.4 - Applied Aerodynamics
INVESTIGATION ON FLOW SEPARATION EFFECTS ON AIRCRAFT LONGITUDINAL MOMENT CHARACTERISTIC FOR FUSELAGE-MOUNTED AIRCRAFT
Y. Zhong¹, Z.-Y. Zhang¹; ¹Shanghai Aircraft Design and Research Institute, China
This paper studies the effects of the wing's different flow separation areas on the low-speed longitudinal moment characteristics.The study will bring more help to the civil aircraft's low speed aerodynamic design.