本站原创论文题目1)(段前30磅,2号黑体,居中)
作者1*,2),作者2+,作者3*,+(小四仿宋,段前1行,行间距16磅,居中)
*(中国科学院力学研究所高温气体动力学国家重点实验室,北京 100190)).. 表1 示例(小5黑体,段前8.5 磅)
序号C反应反应A1氢气燃烧加热氢气燃烧加热O+H2等于H+OH2O+H2等于H+OH5.08×1004A52H+O2等于O+OH3H+O2等于O+OH(6号宋体,单倍行距)
1.2 二级标题
正文.
图1示例
(小五宋体, 段前段后各8.5磅)
2 结 论
正文.
参考文献(5号黑体,段前段后各12磅)
1 Tirres G, Bradley M, Morrison G. Flow Quality Analysis for Future Hypersonic Vehicle Testing.In: Han ZYed.Proc of '97 AETE,Huangshan,1997-10-23～26. Beijing:Science Press,1997.191～199 (小五宋体,行距12磅)(会议论文集格式)
2 Liakopoulos AC. Transient flow though unsaturated porous media. [Ph D Thesis]. University of California,Berkeley,CA,1965 (学位论文格式)
3 章根德. 固体-流体混合物连续介质理论及其在工程上的应用. 力学进展,1993,23(1):58～67 (期刊格式)
4 Lewis RW, Schrefler BA. The finite element method in porous media. New York: Wiley, 1996(出版书籍) RESEARCH ON ANN-BASED PREDICTION MODEL USED TO DOUBLE GLOW SURFACE ALLOYING PROCESSING(12号 Time New Roman加粗 居中,段前30磅,段后12磅)
WANG Er1 LI Xiaosi2(10号 Times New Roman 居中)
(1 Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, C A S, No.15 Beisihuanxi Road, Beijing 100190, China)
(2 Hypersonic Research Center CAS, No.15 Beisihuanxi Road, Beijing 100190, China)New Roman 居中)
Abstract(10号 Time New Roman加粗) Research advances and development of hypersonic vehicles in recent years were reviewed, and relevant technologies of hyersonic vehicles were summarized in the world firstly. Then flight dynamic characteristics in hypersonic vehicles and feasible scheme of TSTO at present were briefly analyzed and summarized. Finally, the methods of hypersonic flight control were reviewed and the future in this field was prospected. (10号 Times New Roman,行距16磅,段前12 磅,段后12磅)
Key words hydrogen burning, hydrogen-ethene , heating methods (10号 Times New Roman)
备注:页边距上下左右均为72磅
中国力学大会-2016
中国力学大会-2016
基金资助项目
2):
1)The project was supported by the (12345678)and (9876543)
2)E-mail: