前言本文评述了导弹气动力快速预测编码的九种技术状态。为了进行详细计算,选取了海军地面武器中心NSWC的气功预测和尼尔森工程与发展中心(NEAR)导弹Ⅱ的编码,对不同外形(“麻雀”Ⅲ、“军队通用化”导弹、“幼南”与“黄蜂”)研究了预测六分量气动力编码的能力。一般当攻角小于10°～15°预测纵向气动力时,两种编码与风洞试验相比,其一致性较好。并为未来导 Preface This paper reviews nine technical states for the rapid aerodynamic prediction of missiles. In order to carry out the detailed calculation, the naval ground weapon center NSWC’s Qigong prediction and the NEAR missile II code were selected. The data of different configurations (“Sparrow III”, “Army Generalized” missiles, “Young South” “Hornets”) studied the ability to predict six-component aerodynamic coding. Generally, when the angle of attack is less than 10 ° ~ 15 ° to predict the longitudinal aerodynamic force, the consistency of the two codes is better than the wind tunnel test. And for the future guide