Author(s)

Yuki Kishi¹, Masahiro Kanazaki¹, Yoshikazu Makino², Kisa Matsushima³

¹Guraduate School of System Design, Tokyo Metropolitan University, Tokyo, Japan.
²Aeronautical Technology Directorate, Japan Aerospace Exploration Agency, Tokyo, Japan.
³Faculty of Engineering, University of Toyama, Toyama, Japan.

In this study, the wing design problem for different planforms for supersonic transport (SST) under supersonic and transonic cruise conditions is discussed to obtain knowledge of the supersonic air-foil from the viewpoint of wing planform dependency. Two types of planforms were considered—a cranked arrow wing with a high sweep-back angle and a tapered wing with a low sweep- back angle. The optimum airfoils of these planforms were designed by efficient global optimization, which combined the evolutionary algorithm with the Kriging surrogate model. To acquire design knowledge, the functional analysis of variance was applied to the solution space and the design space. The design results show that the optimum airfoil and the contribution ratios of design variables for the airfoils of the two planform are different.

Supersonic Wing, Multi-Point Design, Airfoil Design, Knowledge Discovery

Kishi, Y. , Kanazaki, M. , Makino, Y. and Matsushima, K. (2016) Planform Dependency on Airfoil Design Results for Supersonic Wing in Supersonic and Transonic. Journal of Flow Control, Measurement & Visualization, 4, 38-48. doi: 10.4236/jfcmv.2016.41004.