missile aerodynamics 中文意思是什麼
missile aerodynamics
解釋
導彈空氣動力學- missile : n 投射器；飛射器[箭、炮彈等]，射彈，飛彈；導彈。 an air to air （guided） missile 空對空飛彈，機...
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Part, study the model of side jet and aerodynamics compound control intercept missile
第一部分研究了直接力控制攔截導彈的模型。 -
This paper mainly works on the problem of modeling, control and guidance for a side jet and aerodynamics compound control intercept missile
本文的研究主要是圍繞著直接力和氣動力復合控制攔截導彈的建模、控制和制導所展開的。 -
The missile with its radome is at high temperature during the entrance. due to aerodynamics heating process, the high temperature cause air ionization and ablation of the radome, so the radome is at unsymmetrical heat environment, its electrical properties vary with different parts of the radome
導彈在再入過程中，由於空氣動力加熱效應，引起空氣電離和天線罩表面被燒蝕，因此，天線罩處于不對稱熱環境中，它各部分的介電性能不同。 -
Lateral jet control technology is researched in this dissertation, based on supersonic / hypersonic missile aerodynamics and lateral jet interaction ( ji ) effects associated with the attitude control solid - propellant rocket motors system in the low endoatmospheric range
橫向噴流干擾效應研究在超聲速高超聲速導彈總體設計和精確制導技術研究領域一直佔有重要地位。本論文針對大氣層內超聲速高超聲速導彈採用姿態固體火箭發動機側噴流控制技術的一些問題進行了研究。
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