The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.
摘要
一实验电弧加热式发动机二
称亚跨超音速流动
行了数值模拟，所采用的方法是矢
量分裂算法。
arcjet
/'ɑ:kdʒet/
n. 电弧火箭;电弧加热等离子体射流
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行改，
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。
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相似单词
arcifera, arcifinious, arciform, arcilla, arcing, arcjet, arco, arcocentrum, arcograph, arcology,
n. 
火箭;
热等离子体射流
火箭;热等离子体射流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
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
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
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。
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arcifera, arcifinious, arciform, arcilla, arcing, arcjet, arco, arcocentrum, arcograph, arcology,
n. 电弧火箭;电弧加热等离子体射流
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
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.
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。
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相似单词
arcifera, arcifinious, arciform, arcilla, arcing, arcjet, arco, arcocentrum, arcograph, arcology,
n. 火箭;热等离子体射流
火箭;热等离子体射流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
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.
该文在原有热发动机基础上进行改进，设计了覆盖发动机
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
观点；若发现问题，欢迎向我们指正。
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arcifera, arcifinious, arciform, arcilla, arcing, arcjet, arco, arcocentrum, arcograph, arcology,
n. 电弧火箭;电弧加热等离子体射流
The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.
摘要
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。
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arcifera, arcifinious, arciform, arcilla, arcing, arcjet, arco, arcocentrum, arcograph, arcology,
n. 电弧火箭;电弧加热等
射流
射流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
：
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。
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arcifera, arcifinious, arciform, arcilla, arcing, arcjet, arco, arcocentrum, arcograph, arcology,
n. 电弧火箭;电弧加
子体射流
子体射流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
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：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，其表达内容亦不代表本软件的观点；若发现问题，欢迎向我们指正。
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arcifera, arcifinious, arciform, arcilla, arcing, arcjet, arco, arcocentrum, arcograph, arcology,
n. 
箭;加热等离子体射流
箭;加热等离子体射流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
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。
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arcifera, arcifinious, arciform, arcilla, arcing, arcjet, arco, arcocentrum, arcograph, arcology,
n. 火箭;热等离子体射流
火箭;热等离子体射流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.
该文在原有热发动机基础上进行改进，设计了覆盖发动机环形空腔，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观点；若发现问题，欢迎向我们指正。
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arcifera, arcifinious, arciform, arcilla, arcing, arcjet, arco, arcocentrum, arcograph, arcology,