摘要
针对战术技术要求分析的主要问题，以飞机全机重量为核心，对全机重量的计算进行了研究，提出了空机重量和燃油重量的计算方法，得出了满意的结果。经过实际型号的验算，证明本文提出的算法，精度较高，方法可行。
For main problems of tactic-technology requirement analysis, on the basis of analyzing fighter-plane take-off weight, the methods of calculating empty weight and fuel weight are studied in this paper. After contrasting with some fighter plane in existence, the method discussed in this paper is feasible and can be used for tactic-technology requirement analysis.
出处
《航空计算技术》
1999年第4期27-30,共4页
Aeronautical Computing Technique
