远程火箭弹卷弧翼气动载荷工程计算方法  

An Engineering Calculating Method of the Aerodynamic Load for Long Range Rocket Projectile Wrap-Around Wings

作　　者：程养民[1] 

机构地区：[1]中国航天工业总公司四院四十一所,西安710025

出　　处：《固体火箭技术》1997年第4期1-6,共6页Journal of Solid Rocket Technology

摘　　要：根据卷弧翼气动特性，引入各种干扰因素，利用刚体弹道方程计算出卷弧翼的最大气动载荷。经实例验证表明，该方法的计算结果与飞行试验结果是符合的。Using the risid body ballistic equations and considering a number of interference factors,maxdrium aerodynamic load of the wrap-around wings is calculated in accordance with the aerodynamic characteristics of the wings. It is shown by the verifacation of samples that the calculated results by the method agree with the flight tested results.

关 键 词：翼载荷 非对称翼型 气动载荷 卷弧翼 火箭弹 

分 类 号：TJ011.3[兵器科学与技术—兵器发射理论与技术]