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.
前体外形和外界大气密度不变的条件下,提出了利用
炮口
赫数和顶点
赫数确定旋转
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.
前体外形和外界大气密度不变的条件下,提出了利用
炮口
赫数和顶点
赫数确定旋转
最佳尾锥角的方法。
声明:以上例句、词性分类均由互联网资生成,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.
在弹丸前和
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尾锥角的方法。
声明:以上例句、词性分类均由资源自动生成,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条件下,提
用弹丸炮口
赫数和顶点
赫数确定旋转弹丸最佳尾
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
,
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
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,其容亦不代
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
,
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
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
用弹丸炮口
赫数和顶点
赫数确定旋转弹丸最佳尾
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.
在弹丸前体外形和外界大气密的条件下,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、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
代表本软件的观点;若发现问题,欢迎向我们指正。