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基于参数化导波体的乘波体设计和分析

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基准流场的特性是影响乘波体外形和气动特性的核心因素,如何改进基准流场生成更符合需求的乘波体仍然是设计的难题.本文中采用参数化的方法设计导波体外形,并采用激波装配法求解基准流场,通过改变参数控制导波体外形,进而影响基准流场的特性,得到基准流场后,采用"平切激波面"的方法得到乘波面和乘波体.具体分析了导波体的水平面母线形式、钝头半径、下表面底部型线形状对所得乘波体的影响.结果表明:在导波体长宽高一定的情况下,水平面母线采用适当的外扩张形式,可以得到升阻比更大的、压心更靠前的乘波体;钝头半径越大,所得乘波体的升阻比更小,容积率更大,压心更靠前;底部型线外扩张的程度越大,所得乘波体升阻比更小,容积率更大,压心位置差别不大.
Waverider design and analysis based on parametric shock generating body
The characteristics of the reference flow field are the core factors affecting the shape and aerodynamic characteristics of the waverider,and how to generate a waverider that is more in line with the needs by improving the reference flow field is still a design problem.The shape of the shock generating body is designed by parametric method,and the shock-fitting method is used to solve the reference flow field,and the shape of the shock generating body is controlled by changing the parameters,which then affects the characteristics of the reference flow field.The effects of the horizontal busbar form,head passivation radius,and bottom profile shape of the shock generating body on the obtained waverider are analyzed.The results show that under the condition that the shock generating body length,width and height are fixed,the horizontal bus bar adopts the appropriate external expansion form,and the waverider with a larger lift-to-drag ratio can be obtained,and the pressure center is further forward.The larger the radius of the blunt head,the smaller the lift-to-drag ratio of the obtained waverider,the larger the volume ratio,and the pressure center is further forward.The greater the degree of expansion outside the bottom type,the smaller the lift-to-drag ratio of the obtained waverider,the larger the volume ratio,and the difference in the position of the pressure center is not much.

waveridersshock generating bodyvolume ratiohypersonicaerodynamic characteristics

刘小池、何跃龙

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中国航天空气动力技术研究院,北京 100074

乘波体 导波体 容积率 高超声速 气动特性

2024

兵器装备工程学报
重庆市(四川省)兵工学会 重庆理工大学

兵器装备工程学报

CSTPCD北大核心
影响因子:0.478
ISSN:2096-2304
年,卷(期):2024.45(1)
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