The shock wave drag influence from the section area distribution should be considered in supersonic aircraft design,and the aircraft configuration should be adjusted and optimized according to the area rule.To increase the efficiency of supersonic aircraft configuration adjustment,the accurate shapemodified method is researched through the analysis of aircraft section area distribution curve based on the area rule.An aircraft section area distribution curve analysis method is proposed based on automatic are...
【更新日期】
2016-07-27
【分类号】
V223
【正文快照】
引用格式:徐敏,白振东,燕瑛,等.基于面积律自动判别的飞机机身外形修形方法[J].南京航空航天大学学报,2016,48(3):438-444.Xu Min,Bai Zhendong,Yan Ying.Aircraft fuselage configuration adjustment method using automaticjudgment of area rule[J].Journal of Nanjing Univ
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