missile body meaning in English
导弹弹体
导弹壳体
Examples
- This paper analyzes the structural reliability of surfa ce ( ship ) to air missile body , introduced the method of engineering calculation f or structural reliability of missile body and presents a technical way of impro ving structural reliability of missile body
对地(舰)空导弹弹体结构可靠性进行了分析，介绍了弹体结构可靠性的工程计算方法，提出了改进弹体结构可靠性的技术途径。 - Abstract : this paper analyzes the structural reliability of surfa ce ( ship ) to air missile body , introduced the method of engineering calculation f or structural reliability of missile body and presents a technical way of impro ving structural reliability of missile body
文摘:对地(舰)空导弹弹体结构可靠性进行了分析，介绍了弹体结构可靠性的工程计算方法，提出了改进弹体结构可靠性的技术途径。 - According to flight dynamics , a particle model and an attitude model in launching coordinate system and in quasi missile body coordinate system are established , the influence imposed by constant wind , thrust bias of the motor and connection bias are analyzed
应用飞行动力学理论,建立了发射坐标系与准弹体系下助推段和分离过程质点运动和姿态动力学模型,分析常风干扰、发动机推力偏差和装配误差影响等。 - Based on the aerodynamic characteristics of space shuttle booster - like missile bodies at angle of attack from 0 to 180 , the flying characteristics of high maneuver at 90 angle of attack and velocity consuming at 180 angle of attack are analyzed
摘要以新一代无翼式气动布局导弹为背景，在大攻角气动特性理论基础上，分析了在导弹主动段、攻角在180范围内变化的导弹飞行特性，得出了90内大攻角最大转弯能力和180攻角附近最大降速效果的结论。 - Thirdly , this dissertation briefly introduces the engineering estimation method of the aerodynamic heat and supplies the simplified formulas . not considering the rejection , the ablation and some other factors , the author calculates the stagnation heat flux and the non - stagnation field heat flux distribution of some fly situation as the example aerodynamic heat environment . finally , by using the ansys program , the thermal vibration characters of the plate and missile body structures with different materials is analyzed
这一方法提高了热振动的分析效率；第三，简要的介绍了工程上计算气动熟的估算方法及热流密度计算的简化公式，在不考虑烧蚀以及质量引射等影响下，本文计算了几种飞行条件下驻点和非驻点区的热流密度分布，作为本论文算例的气动加热环境。