There is no abstract available for this article.
National Natural Science Foundation of China(11372324)
Institute of Mechanics
Chinese Academy of Sciences(LHD2017TC01)
and the State Key Laboratory of High Temperature Gas Dynamics
This work was supported by the National Natural Science Foundation of China (Grant Nos. 11372324, and 11572333), and the State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences (Grant Nos. LHD2017TC01, LHD2017MS04, and LHD2017QN03).
[1] Chen Z., Yu C. P., Li L., Li X. L.. Sci. China-Phys. Mech. Astron., 2016, 59: 664702 CrossRef ADS Google Scholar
[2] Wang Q., Li J. P., Zhao W., Jiang Z. L.. Sci. China-Phys. Mech. Astron., 2016, 59: 624701 CrossRef ADS Google Scholar
[3] Zhu H., Fu S.. Sci. China-Phys. Mech. Astron., 2017, 60: 104712 CrossRef Google Scholar
[4] Tan S., Li Q. B.. Sci. China-Phys. Mech. Astron., 2017, 60: 114713 CrossRef Google Scholar
[5] Cui K., Hu S. C., Li G. L., Qu Z. P., Situ M.. Sci. China Tech. Sci., 2013, 56: 1980 CrossRef Google Scholar
[6]
D. Küchemann,
[7]
M. A. Lobbia, in
[8] Kontogiannis K., Sóbester A., Taylor N.. J. Aircraft, 2017, 54: 890 CrossRef Google Scholar
[9] Cui K., Yang G. W.. Chin. Sci. Bull., 2007, 52: 57 CrossRef Google Scholar
[10] Cui K., Li G. L., Xiao Y., Xu Y. Z.. AIAA J., 2017, 55: 1909 CrossRef ADS Google Scholar
Figure 1
Configuration and aerodynamic performance comparison between the HIAC and the reference model. (a) HIAC; (b) Ref; (c)
|
|
|
|
|
|
5 |
1.0×106 |
345 |
1.89×103 |
58 |
2.299×107 |
6 |
2.5×106 |
465 |
1.58×103 |
57 |
2.365×107 |
7 |
4.0×106 |
590 |
9.66×102 |
55 |
1.791×107 |
Copyright 2019 Science China Press Co., Ltd. 科学大众杂志社有限责任公司 版权所有
京ICP备18024590号-1