1) orbital average energy
轨道平均能
1.
In this paper,the topological index mY of orbital average energy is proposed.
构建了轨道平均能拓扑指数mYo用mY的0阶指数0Y与80种离子标准生成热ΔfHθm进行关联,拟合的回归方程的相关系数为0。
2) average energy of valence orbits
价层轨道平均能
1.
It is found that the average values of average energy of valence orbits parameters defined either as an average of energy of valence orbit for cations and anions taken together or as the difference between the averages of energy of valence orbit for cations and anions taken separately concentrate in a narrow range for about 60 superconducting copper oxides.
研究了各种类型的氧化铜的高温超导电性与原子价层轨道能的关系，发现在６０种氧化铜超导体中，不管是全部阳离子和阴离子的价层轨道平均能的平均值或是阳离子的价层轨道平均能的平均值与阴离子的价层轨道平均能的平均值之差都集中在一个狭窄的范围。
2.
The criterion shows that the average values of average energy of valence orbits of atom of all the oxide superconductors concentrate in a narrow range from -12.
判据指出，一切氧化物超导体的原子价层轨道平均能的平均值都在－１２。
3) average energy of valence orbitals
价层轨道平均能
1.
In this paper, an equation is obtained through researching the reqularity of the vibrational frequency of the Chemical bond A-H by using the average nuclear potential of the valence electrons and the average energy of valence orbitals.
本文用价层轨道平均能和价电子的平均核势来研究 A- H键振动频率的规律性 ,得出了一个关系式 ,用此公式计算振动频率的值与实验值非常接
2.
A formula to show the relationship between tlie vibrational frequency V_(X-H)and the bondlength, the average energy of valence orbitals is suggested in the present paper:The formula has been used to calculate the vibrational frequcency V_(X-H) of some familiar covalent molecular hydrides.
本文给出了振动频率Ｖ＿（ｘ－Ｈ）与价层轨道平均能，键长的关系方程：。
4) energy of valence orbit
价层轨道平均能
1.
The correlation between the energy of valence orbit and the critical current density of doping MgB2 was researched in this paper.
本文研究了掺杂二硼化镁超导体系的原子价层轨道平均能|M|与临界电流密度Jc之间的关系,发现它们之间有较好的规律性。
6) mean orbit
平均轨道
1.
On the basis of mean orbit concept,a fast algorithm for the prediction of LEO satellite passes and image opportunity is presented.
在引入平均轨道概念的基础上,提出了一种针对低轨道卫星的过顶与成像区域时间的快速预报算法。
2.
An orbital modulation method by controlling the corresponding transient orbit errors of mean orbit control targets was proposed.
提出了一种通过控制平均轨道控制目标对应的瞬时轨道偏差量进行轨道修正的方法。
补充资料：轨道保持(见航天器轨道控制)
轨道保持(见航天器轨道控制)
orbit keeping
guidQo baoehi轨道保持(o rbit keePing)见航天器轨道控制。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条