The aviation bomb is flying in the high density atmosphere layer. Its fight Mach number is generally 0.9.
航弹主要是在稠密的大气层中飞行,巡航马赫数一般在0.9附近。
参考来源 - 某型号制导航弹气动外形设计及机弹分离气动特性研究The result is among the best ones in our country. And it provides reliable gist for analyzing the dynamic parameter of rocket bomb.
结果表明，测量的相对误差小于1％，达到国内先进水平，为分析航弹动态参数，提供了可靠的依据。
参考来源 - 航弹极转动惯量测试原理研究·2,447,543篇论文数据，部分数据来源于NoteExpress
航弹主要是在稠密的大气层中飞行，巡航马赫数一般在0.9附近。
The aviation bomb is flying in the high density atmosphere layer. Its fight Mach number is generally 0.9.
根据非平静大气下弹箭运动方程组，针对航弹在风影响作用下产生的落点散布，采用脉冲修正方式对航弹落点偏差进行风校正。
According to the motion equation in the non-quietude atmosphere, the authors calculate the dispersions of bomb on the effect of the wind have adopt and the pattern of the impulse correction.
该文研究各种航姿算法对常规弹箭高动态运动特征的适应性。
The applicability of kinds of attitude algorithms's to highly dynamic character of rocket are discussed in this paper.
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