Flow Dominating Instability in Supersonic Flows
Author:
Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-15-3595-6_3
Reference46 articles.
1. Mohieldin, T. O., Tiwari, S. N., & Olynciw, M. J. (2001). Asymmetric flow-structures in dual mode scramjet combustor with significant upstream interaction. In 37th AIAA/ASME/SAE/ASEE Jet Propulsion Conference & Exhibit (p. 3296). AIAA.
2. Rodriquez, C. (2001). Asymmetry effects in numerical simulation of supersonic flows with upstream separated regions. In 39th Aerospace Sciences Meeting and Exhibit (p. 84). AIAA.
3. Gao, T., Liang, J., Sun, M., & Zhong, Z. (2017). Dynamic combustion characteristics in a rectangular supersonic combustor with single-side expansion. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 231(10), 1862–1872.
4. Sun, M.-B., Zhong, Z., Liang, J.-H., & Wang, Z.-G. (2014). Experimental investigation of supersonic model combustor with distributed injection of supercritical kerosene. Journal of Propulsion and Power, 30(6), 1537–1542.
5. Ouyang, H., Liu, W., & Sun, M. (2016). Parametric study of combustion oscillation in a single-side expansion scramjet combustor. Acta Astronautica, 127, 603–613.
1.学者识别学者识别
2.学术分析学术分析
3.人才评估人才评估
"同舟云学术"是以全球学者为主线，采集、加工和组织学术论文而形成的新型学术文献查询和分析系统，可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容，当前同舟云学术共收录了国内外主流学术期刊6万余种，收集的期刊论文及会议论文总量共计约1.5亿篇，并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询！咨询电话：010-8811{复制后删除}0370
www.globalauthorid.com
TOP
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3