基于灰色田口法的飞行器减阻降热研究与优化设计

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中图分类号：035;V411.3 文献标志码：A 文章编号：1000-4939（2025）06-1254-09

Abstract： Hypersonic aircraft face extremely high aerodynamic resistance and heating during flight， posing a threat to flight safety and stability.Taguchi-gray correlation method is utilized to study the impact of size on the resistance and heat reduction performance of hypersonic aircraft. An orthogonal test is conducted， wherein design factors such as spike length-diameter ratio，airway diameter ratio，pneumatic disk diameter ratio，and lateral jet angle are considered.The response targets comprise total flight resistance，peak pressure coefficient，and Stanton number.Test results are obtained through numerical simulation.The findings indicate that the flight resistance is most significantly affected by the length-diameter ratio of the spike，while the lateral jet angle has the least effect.In regard to the peak pressure coeffcient and Stanton number，the size factors exhibit a similar rank of influence.Among these factors，the length-diameter ratio of the pneumatic disk exerts the most significant impact.Increasing the length-diameter ratio of the spike and the diameter ratio of the pneumatic disk can effctively improve overall resistance and heat reduction performance.However，it should be noted that as the size increases，the lifting eficiency gradually diminishes.In comparison to the optimal group of orthogonal design，the optimized configuration demonstrates an overall performance improvement of 4.6% ，thus indicating a favorable optimization effect.

Key words ： numerical simulation; Taguchi method; gray correlation; hypersonic aircraft;reduce drag and heat

高超声速飞行器[]以速度快、突防能力强等优势被世界各国重视，具有重要的军事战略意义和广泛的民用前景[2]。（剩余13918字）