On condition that the front body shape of the projectile is unchangeable,a formula is obtained for determining the relation between the optimum boattail angle and the supersonic flight region.
在弹外形和外界大气密度不变的条件下,提出了利用弹
炮口
赫数和顶点
赫数确定旋转弹
最佳尾锥角的方法。
On condition that the front body shape of the projectile is unchangeable,a formula is obtained for determining the relation between the optimum boattail angle and the supersonic flight region.
在弹外形和外界大气密度不变的条件下,提出了利用弹
炮口
赫数和顶点
赫数确定旋转弹
最佳尾锥角的方法。
声明:以上例句、词性分类均由互联自动生成,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
On condition that the front body shape of the projectile is unchangeable,a formula is obtained for determining the relation between the optimum boattail angle and the supersonic flight region.
在弹丸前体界大气密度不变的条件下,提出了利用弹丸炮口
赫数
顶点
赫数确定旋转弹丸最佳尾锥角的方法。
声明:以上例句、词性分类联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
On condition that the front body shape of the projectile is unchangeable,a formula is obtained for determining the relation between the optimum boattail angle and the supersonic flight region.
在前体外形和外界大气密度不变的条件下,提出了利用
赫数和顶点
赫数确定旋转
佳尾锥角的方法。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
On condition that the front body shape of the projectile is unchangeable,a formula is obtained for determining the relation between the optimum boattail angle and the supersonic flight region.
在丸前体外形和外界大气密度不变的条件下,提出了利用
丸炮
数和顶点
数确定
丸最佳尾锥角的方法。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
On condition that the front body shape of the projectile is unchangeable,a formula is obtained for determining the relation between the optimum boattail angle and the supersonic flight region.
在弹丸前体外形和外界大气密度不变的条件下,提出了利用弹丸炮口赫数和顶点
赫数确定旋转弹丸最佳
角的方法。
声明:以上例句、词性分类均由互联网资源自动生成,分未
工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
On condition that the front body shape of the projectile is unchangeable,a formula is obtained for determining the relation between the optimum boattail angle and the supersonic flight region.
在弹丸前体外形和外界大气密度不变条件下,提出了利用弹丸炮口
赫数和顶点
赫数确定旋转弹丸最佳
角
方法。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经审核,其表达内容亦不代表本软件
观点;若发现问题,欢迎向我们指正。
On condition that the front body shape of the projectile is unchangeable,a formula is obtained for determining the relation between the optimum boattail angle and the supersonic flight region.
在丸前体外形和外界大气密度不变
条件下,提出了利用
丸炮口
赫数和顶点
赫数确定旋转
丸最佳尾锥角
方法。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人,其表达内容亦不代表本软件
观点;若发现问题,欢迎向我们指正。
On condition that the front body shape of the projectile is unchangeable,a formula is obtained for determining the relation between the optimum boattail angle and the supersonic flight region.
在丸前体外形和外界大气密度不变的条件下,提出了
丸炮口
赫数和顶点
赫数确定旋转
丸最
角的方法。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
On condition that the front body shape of the projectile is unchangeable,a formula is obtained for determining the relation between the optimum boattail angle and the supersonic flight region.
在弹丸前体外形和外密度不变的条件下,提出了利用弹丸炮口
赫数和顶点
赫数确定旋转弹丸最佳尾锥角的方法。
声明:以上例句、词均由互联网资源自动生成,部
未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
On condition that the front body shape of the projectile is unchangeable,a formula is obtained for determining the relation between the optimum boattail angle and the supersonic flight region.
在前体外形和外界大气密度不变的条件下,提出了利用
赫数和顶点
赫数确定旋转
佳尾锥角的方法。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。