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浏览/检索结果: 共10条，第1-10条 帮助 限定条件 发表日期：2009     已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序 Configuration optimization of hypersonic vehicles under transitional flow conditions 会议论文 16th AIAA/DLR/DGLR International Space Planes an Hypersonic Systems and Technologies Conference, Germany, Bremen, 2009-10 作者:  Sun QH(孙泉华);  Fan J(樊菁);  Jiang JZ(蒋建政);  Cui K(崔凯);  Sun QH(孙泉华) 收藏  |  浏览/下载：891/150  |  提交时间：2009/12/28 Variation character of stagnation point heat flux for hypersonic pointed bodies from continuum to rarefied flow states and its bridge function study 期刊论文 Science in china series g-physics mechanics & astronomy, 2009, 卷号: 52, 期号: 12, 页码: 2007-2015 作者:  Wang ZhiHui;  Bao Lin;  Tong BingGang 收藏  |  浏览/下载：18/0  |  提交时间：2019/05/10 Rarefied gas effects  Sharp leading edge  Hypersonic  Stagnation point heat flux  Bridge function   Mechanism of unsteady aerodynamic heating with sudden change in surface temperature 期刊论文 Applied mathematics and mechanics-english edition, 2009, 卷号: 30, 期号: 2, 页码: 163-174 作者:  Chen, Hao;  Bao, Lin 收藏  |  浏览/下载：19/0  |  提交时间：2019/05/10 Unsteady aerodynamic heating  Hypersonic  Unsteady surface temperature  Approximate analysis  Numerical simulation   Experimental investigation of hypersonic flow induced separation over double wedges 期刊论文 JOURNAL OF THERMAL SCIENCE, 2009, 卷号: 18, 期号: 3, 页码: 220,225 Tokitada Hashimoto 收藏  |  浏览/下载：10/0  |  提交时间：2013/01/09 Experimental investigation of hypersonic flow induced separation over double wedges 期刊论文 JOURNAL OF THERMAL SCIENCE, 2009, 卷号: 18, 期号: 3, 页码: 220,225 作者:  Tokitada Hashimoto 收藏  |  浏览/下载：16/0  |  提交时间：2013/01/09 Flow-field of the excited jet and mixing in the supersonic flow 会议论文 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009 作者:  Gu SL(顾声龙);  Chen LH(陈立红);  Gu HB(顾洪斌);  Li F(李飞);  Wei Z(卫喆) 收藏  |  浏览/下载：11/0  |  提交时间：2017/07/14 Different frequency  Gas sampling  Hartmann  Jet devices  Large-scale structure  Planar laser  Shear layer  Total-pressure loss   Aerodynamic characteristics research on wide-speed range waverider configuration 期刊论文 Science in China Series E-Technological Sciences, 2009, 卷号: 52, 期号: 10, 页码: 2903-2910 作者:  Wang FM(王发民);  Ding HH(丁海河);  Lei MF(雷麦芳);  Wang FM;  Wang FM 收藏  |  浏览/下载：876/195  |  提交时间：2009/08/03 Waverider Configuration  Aerodynamic Characteristics At Wide-Speed Range  High Lift-To-Drag Ratio   Performance of the fuel injector in supersonic combustor 会议论文 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009 作者:  Wei Z(卫喆);  Chen LH(陈立红);  Gu HB(顾洪斌);  Li F(李飞);  Gu SL(顾声龙) 收藏  |  浏览/下载：16/0  |  提交时间：2017/07/14 Concentration profiles  Engine design  Fuel injectors  Fuel-air mixing  Gas sampling  Ramp injector  Scramjet combustors  Scramjet test  Supersonic combustors   Design of Base Flow for Streamline-Traced Hypersonic Inlet 会议论文 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, International Space Planes and Hypersonic Systems and Technologies Conferences, Bremen, Germany, 19 October 2009 - 22 October 2009 作者:  Yue LJ(岳连捷);  Xiao YB;  Chen LH(陈立红);  Chang XY(张新宇) 收藏  |  浏览/下载：10/0  |  提交时间：2017/06/01 郭永怀文集 专著 北京:科学出版社, 2009 郭永怀 收藏  |  浏览/下载：1629/71  |  提交时间：2009/07/03