These shotty nodes are usually firm, not fixed, and are less than a centimeter in diameter.
这些似样结节通常坚硬,不固定,直径小于1厘米。
These shotty nodes are usually firm, not fixed, and are less than a centimeter in diameter.
这些似样结节通常坚硬,不固定,直径小于1厘米。
In this paper , pill-setover control system which used for incept and disposal of signal of space movement is devised and explored in detail.
本文对制系统空间运动信号的接收与处理进行了全面的设计与探索。
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
外界大气密度不变的条件下,提出了利用
炮口马赫数
顶点马赫数确定旋
最佳尾锥
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。
These shotty nodes are usually firm, not fixed, and are less than a centimeter in diameter.
这些似样结节通常坚硬,不固定,直径小于1厘米。
In this paper , pill-setover control system which used for incept and disposal of signal of space movement is devised and explored in detail.
本文对偏角控制系统空间运动信号的接收与
行了全面的设计与探索。
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
外界大气密度不变的条件下,提出了利用
口马赫数
顶点马赫数确定旋转
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。
These shotty nodes are usually firm, not fixed, and are less than a centimeter in diameter.
这些似弹丸样结节通,不固定,直径小于1厘米。
In this paper , pill-setover control system which used for incept and disposal of signal of space movement is devised and explored in detail.
本文对弹丸偏角控制系统空间运动信号的接收与处理进行了全面的设计与探索。
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.
在弹丸前体外形外界大气密度不变的条件下,提出了利用弹丸炮口马赫数
顶点马赫数确定旋转弹丸最佳尾锥角的方法。
声明:以上例句、词类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。
These shotty nodes are usually firm, not fixed, and are less than a centimeter in diameter.
这些似样结节通常坚硬,不固定,直径小于1厘米。
In this paper , pill-setover control system which used for incept and disposal of signal of space movement is devised and explored in detail.
本文对偏角控制系统空间运动信号的接收与处理进行了全面的设计与探索。
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.
在体外形
外界大
不变的条件下,提出了利用
炮口马赫数
顶点马赫数确定旋转
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。
These shotty nodes are usually firm, not fixed, and are less than a centimeter in diameter.
这些似弹丸样结节通常坚硬,固定,直径小于1厘米。
In this paper , pill-setover control system which used for incept and disposal of signal of space movement is devised and explored in detail.
本文对弹丸偏角控制系统空间运动信号接收与处理进行了全面
设计与
。
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.
弹丸前体外形
外界大气密度
条件下,提出了利用弹丸炮口马赫数
顶点马赫数确定旋转弹丸最佳尾锥角
方法。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦代表本软件
观点;若发现问题,欢迎向我们指正。
These shotty nodes are usually firm, not fixed, and are less than a centimeter in diameter.
这些似弹丸样结节通常坚硬,不固定,直径小于1厘米。
In this paper , pill-setover control system which used for incept and disposal of signal of space movement is devised and explored in detail.
本文对弹丸偏角控制系统空间运动信号接收与处理进行了全面
与探索。
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.
在弹丸前体外形外界大气密度不变
条件
,
出了利用弹丸炮口马赫数
顶点马赫数确定旋转弹丸最佳尾锥角
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。
These shotty nodes are usually firm, not fixed, and are less than a centimeter in diameter.
这些似弹样结节通常坚硬,不固定,直径小于1厘米。
In this paper , pill-setover control system which used for incept and disposal of signal of space movement is devised and explored in detail.
本文对弹偏角控制系统空间运动信号的接收与处理进行了全面的设计与探索。
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
外界
度不变的条件下,提出了利用弹
炮口马赫数
顶点马赫数确定旋转弹
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。
These shotty nodes are usually firm, not fixed, and are less than a centimeter in diameter.
这些似弹丸样结节通常坚硬,不固定,直径小于1厘米。
In this paper , pill-setover control system which used for incept and disposal of signal of space movement is devised and explored in detail.
本文对弹丸偏角控制系统空间运动信号的接收与处理进面的设计与探索。
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.
在弹丸前体外形外界大气密度不变的条件下,提出
弹丸炮口马赫数
顶点马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。
These shotty nodes are usually firm, not fixed, and are less than a centimeter in diameter.
这些似样结节通常坚硬,不固定,直径小于1厘米。
In this paper , pill-setover control system which used for incept and disposal of signal of space movement is devised and explored in detail.
本文对偏角控制系统空间运动信号的接收与处
了全面的设计与探索。
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
外界大气密度不变的条件下,提出了利
炮口马赫数
顶点马赫数确定旋转
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。