Investigation of the tail dihedral effects on the aerodynamic characteristics for the low speed aircraft.
Zhang, G. Q.
Yu, S. C. M.
Date of Issue2013
School of Mechanical and Aerospace Engineering
The aerodynamic characteristics for the vee-tail aircraft configuration have been investigated numerically at low Reynolds number (Re < 10 6). Three types of vee-tails have been adopted to be compared with the conventional tail type (with horizontal and vertical tails).The results show that the effect created by the vee-tail can greatly affect the aerodynamic characteristics of the whole aircraft. If the dihedral angle of the vee-tail is too large, it can directly affect the flight stability. The main reason for the longitudinal moment curve “moving up” at high dihedral angle can be attributed to the serious asymmetric downwash effect. Based on these, the force variation and the corresponding aerodynamic characteristics for three different sizes of aileron with different deflection angles have also been obtained computationally and analyzed in detail.
Advances in mechanical engineering
© 2013 The Author(s). This paper was published in Advances in Mechanical Engineering and is made available as an electronic reprint (preprint) with permission of The Author(s). The paper can be found at the following official DOI: [http://dx.doi.org/10.1155/2013/308582]. One print or electronic copy may be made for personal use only. Systematic or multiple reproduction, distribution to multiple locations via electronic or other means, duplication of any material in this paper for a fee or for commercial purposes, or modification of the content of the paper is prohibited and is subject to penalties under law.