Center Body Airfoil Design for Blended Wing Body Configuration

To design the center-body airfoil of a blended wing body configuration, the aerodynamic effects of the symmetrical airfoil, trailing-edge reflexed airfoil, leading-edge loaded airfoil and leading-edge loaded plus trailing-edge reflexed airfoil are investigated based on the constraints of system arra...

詳細記述

書誌詳細

出版年:	Xibei Gongye Daxue Xuebao
フォーマット:	論文
言語:	中国語
出版事項:	EDP Sciences 2018-04-01
主題:	airfoils wings computational fluid dynamics design aerodynamic configurations lift drag ratio blended wing body civil transport unmanned aerial vehicles(uav)
オンライン･アクセス:	https://www.jnwpu.org/articles/jnwpu/pdf/2018/02/jnwpu2018362p203.pdf