32th Congress of the International Council of the Aeronautical Sciences

03.4 - Applied Aerodynamics

AERODYNAMIC DESIGN OPTIMIZAITON OF HYPERSONIC WING OVER WIDE MACH-NUMBER RANGE CONSIDERING LIFT MATCHING

Y. Zhang¹, Z.-H. Han¹, F. Liu¹, C.-Z. Xu¹; ¹Northwestern Polytechnical University, China

This paper carries out aerodynamic shape design optimization of wide-mach-number-range wing considering lift matching based on surrogate models. The optimization considers both planar shape and profile shape optimization and gets some optimal wings. With these optimization results, design criteria of wide-mach-number-range wing considering lift matching are summarized.


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