Effect of fuselage diameter on aerodynamic characteristics for straight wing at low and high aspect ratio

International Conference on Aerospace and Mechanical Engineering 2017

航空航天工程;机械制造

Lai, H.C.^1 ; Kamaruddin, N.M.^1

School of Aerospace Engineering, Engineering Campus, Universiti Sains Malaysia, Nibong Tebal, Penang

14300, Malaysia^1

关键词: Aerodynamic characteristics;    Computational codes;    Computational results;    Drag prediction;    High aspect ratio;    Lift and drag coefficients;    Lifting Line Theory;    Wing aspect ratio;   

Others  :  https://iopscience.iop.org/article/10.1088/1757-899X/370/1/012055/pdf
DOI  :  10.1088/1757-899X/370/1/012055

学科分类：航空航天科学

来源: IOP

【 摘 要 】

A computational code has been developed to investigate the effect of fuselage diameter with a combination of a straight wing on the aerodynamic characteristics. The case studies were performed on both wing-body combination at high wing aspect ratio (AR>4) and low wing aspect ratio (AR