Thrust and Drag of a Scramjet Model with Different Combustor Geometries

机译：具有不同燃烧器几何形状的Scramjet模型的推力和阻力

获取原文

页面导航

著录项
相似文献
相关主题

著录项

来源
《AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference》|2005年|P.1-8|共8页
会议地点 Capua(IT)
作者
X. Chang; H. Gu; L. Chen;
展开▼
作者单位

Chinese Academy of Sciences, Beijing, China (prc);

Chinese Academy of Sciences, Beijing, China (prc);

Chinese Academy of Sciences, Beijing, China (prc);

展开▼
会议组织
原文格式 PDF
正文语种
中图分类各类型航空器;
关键词
入库时间 2022-08-26 14:19:42

相似文献

外文文献
中文文献
专利

1. Thrust control strategy based on the minimum combustor inlet Mach number to enhance the overall performance of a scramjet engine [J] . Ji Zifei, Zhang Huiqiang, Wang Bing Proceedings of the Institution of Mechanical Engineers . 2019,第13期

机译：基于最小燃烧器进气口马赫数的推力控制策略可增强超燃冲压发动机的整体性能
2. Experimental study on combustion modes and thrust performance of a staged-combustor of the scramjet with dual-strut [J] . Yang Qingchun, Chetehouna Khaled, Gascoin Nicolas, Acta astronautica . 2016,第MayaJuna期

机译：双支柱超燃冲压发动机分级燃烧器燃烧模式和推力性能的实验研究
3. Control of Thrust characteristics of a Scramjet Combustor with Vibrational combustion Using Acoustic Resonators [J] . V.K. Baev, D.Yu. Moskvichev, A.V. Potapkin Combustion, Explosion, and Shock Waves . 2000,第5期

机译：利用声谐振器控制具有振动燃烧的超燃冲压发动机燃烧器的推力特性
4. Thrust and Drag of a Scramjet Model with Different Combustor Geometries [C] . American Institute of Aeronautics and Astronautics/CIRA International Space Planes and Hypersonics Systems and Technologies Conference . 2005

机译：用不同的燃烧室几何形状推力和拖动拼车模型
5. Three-dimensional evolution of a fold-thrust belt salient: Insights from a study of the geometry, kinematics and mechanics of the Provo salient, Sevier Belt, Utah, and from three-dimensional finite element modeling. [D] . Kwon, Sanghoon. 2004

机译：褶皱冲断带凸起的三维演化：从对犹他州Sevier Belt的Provo凸起的几何学，运动学和力学的研究以及三维有限元建模中获得的见解。
6. Investigations on the Influence of the In-Stream Pylon and Strut on the Performance of a Scramjet Combustor [O] . Hao Ouyang, Weidong Liu, Mingbo Sun -1

机译：流内塔架和支柱对超燃冲压燃烧器性能的影响研究
7. Thrust and Drag of a Scramjet Model with Different Combustor Geometries [O] . Xinyu Chang, Hongbin Gu, Lihong Chen 2005

机译：用不同的燃烧室几何形状推力和拖动拼车模型
8. Priori Analysis of Flamelet-Based Modeling for a Dual-Mode Scramjet Combustor. [R] . Quinlan, J. R., McDaniel, J. C., Drozda, T. G., 2014

机译：基于Flamelet的双模式超燃冲压发动机燃烧室建模的先验分析。

Thrust and Drag of a Scramjet Model with Different Combustor Geometries

著录项

相似文献

相关主题

期刊订阅