摘要
本文在试验与理论分析的基础上,建立了飘带—弹体组合体气动力计算的数学模型,导出了飘带式子弹气动力工程计算公式。计算结果表明与实验值是相当一致的,这说明本方法可行。
On the basis of experimental and theoretical analyses the present paper gives a mathematical model for the aerodynamic calculations of a ribbon-body complex, and a method for its aerodynamic engineering calculations. The computed results as shown in the examples, agree well with the experimental values, and show the parcticability of the present method.
出处
《兵工学报》
EI
CAS
CSCD
北大核心
1991年第4期75-82,共8页
Acta Armamentarii
