The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.
摘要对一实验电弧式发动机二维轴对称亚跨超音速流动进行了数值模拟,所采用的方法是矢
量分裂算法。
The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.
摘要对一实验电弧式发动机二维轴对称亚跨超音速流动进行了数值模拟,所采用的方法是矢
量分裂算法。
An annular cavity placed around the anode of arcjet was designed to form a regenerative cooling channel on the base of an arc jet.
该文在原有电弧发动机基础上进行改进,设计了覆盖发动机阳极的环形空腔,形成再生冷却
道。
声明:以上、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。
The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.
摘要对一实验电弧加热式发动机二维轴对称亚跨超音速流动进行了数值模拟,所采用的方法是矢量分裂算法。
An annular cavity placed around the anode of arcjet was designed to form a regenerative cooling channel on the base of an arc jet.
该文在原有电弧加热发动机基础进行改进,设计了覆盖发动机阳极的环形空腔,形成再生冷却
道。
声明: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。
The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.
摘要对一实验电弧加热式发机二维轴对称亚跨超音速流
进行了数值模拟,所采用的方法是矢
量分裂算法。
An annular cavity placed around the anode of arcjet was designed to form a regenerative cooling channel on the base of an arc jet.
该文在原有电弧加热发机基础上进行改进,设计了覆盖发
机阳极的环形空腔,形成再生冷却
道。
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。
The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.
摘要对一实验加热式发动机二维轴对称亚跨超音速流动进行了
拟,所采用的方法是矢
量分裂算法。
An annular cavity placed around the anode of arcjet was designed to form a regenerative cooling channel on the base of an arc jet.
该文在原有加热发动机基础上进行改进,设计了覆盖发动机阳极的环形空腔,形成再生冷却
道。
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。
The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.
摘要对一实验电弧加热式发动机二维轴对称亚跨超音速流动进行了数值模拟,所采用的方法是矢量分裂算法。
An annular cavity placed around the anode of arcjet was designed to form a regenerative cooling channel on the base of an arc jet.
该文在原有电弧加热发动机基础上进行改进,设计了覆盖发动机阳极的环形空腔,形成再生冷却道。
:
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。
The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.
摘要对一实验电弧加热式发动轴对称亚跨超音速流动进行
数值模拟,所采用的方法是矢
量分裂算法。
An annular cavity placed around the anode of arcjet was designed to form a regenerative cooling channel on the base of an arc jet.
该文在原有电弧加热发动基础上进行改进,设
盖发动
阳极的环形空腔,形成再生冷却
道。
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。
The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.
摘要对一实验电弧加热式发动机二维轴对称亚跨超音速流动进行了数值,所采用的方法是矢
量分裂算法。
An annular cavity placed around the anode of arcjet was designed to form a regenerative cooling channel on the base of an arc jet.
该文有电弧加热发动机基础上进行改进,设计了覆盖发动机阳极的环形空腔,形成再生冷却
道。
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。
The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.
摘实验电弧加热式发动机二维轴
称亚跨超音速流动进行了数值模拟,所采用的方法是矢
量分裂算法。
An annular cavity placed around the anode of arcjet was designed to form a regenerative cooling channel on the base of an arc jet.
该文在原有电弧加热发动机基础上进行改进,设计了覆盖发动机阳极的环,
成再生冷却
道。
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。
The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.
摘要对一实验电弧加热式发动机二维轴对称亚跨超音速流动进行了数值模拟,所采用的法
矢
量
法。
An annular cavity placed around the anode of arcjet was designed to form a regenerative cooling channel on the base of an arc jet.
该文在原有电弧加热发动机基础上进行改进,设计了覆盖发动机阳极的环形空腔,形成再生冷却道。
声明:以上例句、词性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。