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1)  mock bomb
模型弹
2)  spring model
弹簧模型
1.
The relation of lateral displacement of bucket top with horizontal loads is obtained based on a soil-spring model.
根据土体的简化弹簧模型,建立了单桶和四桶结构在横向载荷作用下力系的平衡方程,提出了估算水平载荷作用下桶顶水平位移的方法,并将桶顶位移的估算结果同三维有限元方法的数值计算结果进行了比较,发现两者相当一致。
2.
Based on the foundation of spring model of concentrating force in documents[1,2], the calculation method considering effects between springs of concentrating force was given.
在集中力弹簧模型的基础上,给出了集中力弹簧之间考虑相互影响的计算方法、考虑相互影响及不考虑相互影响力弹簧模型的算例,以及工程实例的计算与实测结果的比较。
3)  spring model
弹跳模型
1.
On-line application of spring model in plate rolling process;
中厚板轧机弹跳模型的在线应用
4)  elasticity model
弹性模型
1.
The elasticity model about submarine′s moving (images u)nder water is established, and the matching algorism between submarine′s moving images based on the net of elasticity is studied and (realized.
利用真正物理意义上的弹性模型来解决潜体运动图像变体匹配的问题,建立了海水介质中潜体运动图像的弹性模型,研究和实现了基于弹性网的潜体运动图像匹配算法。
5)  Trajectory model
弹道模型
1.
On the basis of further studying and analyzing the trajectory trait,the paper has constructed fold line trajectory model which is correspond to the flying character of red land laser terminal-guided projectile when firing at near distance.
在分析末制导炮弹外弹道特征的基础上,构建了与末制导炮弹行"近区域"射击时的外弹道特征较符合的"折线法"弹道模型,并用之决定末制导炮弹射击诸元。
2.
Impulse correction scheme of a terminal correction rocket was put forward,and the trajectory model was established.
提出了一种末段修正火箭弹的脉冲修正方案,建立了相应的弹道模型;对单个脉冲发动机的修正能力及修正时机进行了仿真研究;提出了末段多级修正的方法,并对多级修正进行了弹道数字仿真。
3.
It constructed the anti-ship whole trajectory model with interferences,then designed the flight test region by setting missile parameters,contrasted the simulation test with the actual range test,and verified the rationality and superiority of the scheme.
探讨了4个影响飞行航区划定因素:舰面干扰、风干扰、陀螺漂移干扰、导弹故障干扰,构建了反舰导弹干扰作用下的全弹道模型。
6)  aeroelastic model
气弹模型
1.
Wind tunnel test on aeroelastic model of long span transmission line system;
大跨越输电塔线体系气弹模型风洞试验
2.
Identification of flutter derivatives of full-bridge aeroelastic model;
全桥气弹模型颤振导数识别
3.
Analysis of the aerodynamic divergence of an aeroelastic model of Sutong Bridge;
苏通大桥气弹模型气动失稳分析
补充资料:半硬壳式弹体(见弹道导弹弹体)


半硬壳式弹体(见弹道导弹弹体)
semi-hard-shelled missile body

bQn yingkeshi dan桩半硬壳式弹体(semi一hard一shelled、ssilebody)见弹道导弹弹体。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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