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1)  tab assembly
翼片组合
2)  combined fence
组合翼刀
1.
The sketches of secondary flow structure in compressor cascade with endwall fences,blade fences and combined fences were presented.
给出了具有端壁翼刀、吸力面翼刀和组合翼刀的可控扩散叶型(CDA)压气机叶栅的二次流结构简图。
3)  combined wing
组合翼
1.
The results show that the lift and drag characteristics of combined wings are better than simple wings both in and out of ground effect, and that the combined wings are fit for sea-skimming and high-flying WIG craft.
得到的组合翼在地效区内外比简单地效翼具有更好的升阻特性的结果,表明组合翼布局适合于掠海高飞型地效翼艇,研究也为地效翼布局型式、外形参数选择以及吹风模型制作提供了依据。
4)  wing-tail combination
机翼-尾翼组合体
1.
The boundary element method based on Green s law is presented in this paper for the computation of wing-tail combination s unsteady response to gust.
本文以Green函数为基础的边界元法,结合时间历程法,计算机翼-尾翼组合体对突风动态响应的气动性能。
2.
The boundarv element method based on Green theorem is presented in this paper for the computation of supersonic unsteady aero-dynamic forces of wing-tail combinations.
本文以Green函数为基础的边界元,应用时间历程法,计算机翼-尾翼组合体的非定常气动性能。
5)  wing-tail combination
机翼尾翼组合
6)  the wing of aluminium alloy
铝合金翼片
补充资料:组合模式或组合振动
分子式:
CAS号:

性质:在红外光谱中通常出现很多的弱吸收,组合模式或组合振动系指对应于两个或多个基本振动频率之和起源,它的弱吸收于多原子分子振动态相互作用的振子的非谐性。与基频振动及倍频所引起的吸收相比,这些吸收是比较弱的。

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