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,所采用的方法是矢通量分裂算法。
The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.
摘要对一实验电弧加热式机二维轴对称亚跨超音速流
进行了数值模拟,所采用的方法是矢通量分裂算法。
An annular cavity placed around the anode of arcjet was designed to form a regenerative cooling channel on the base of an arc jet.
在原有电弧加热
机
础上进行改进,设计了覆
机阳极的环形空腔,形成再生冷却通道。
has multifarious effects on arcjet thruster operation, and both specific impulse and thrust efficiency can be improved by increasing it befittingly under steady arc.
研究表明,集气腔总压对推力器工作过程具有多方面的影响,在保证电弧稳定的情况下,适当提高集气腔总压可同时提高比冲和推进效率。
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