Assessment of the hypersonic intake isolator and performance evaluation at various flight conditions
Author:
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s42401-024-00316-y.pdf
Reference32 articles.
1. Dalle DJ, Fotia ML, Driscoll JF (2010) Reduced-order modeling of two-dimensional supersonic flows with applications to scramjet inlets. J Propul Power 26(3):545–555. https://doi.org/10.2514/1.46521
2. Torrez SM, Driscoll JF, Dalle DJ, Bolender MA, Doman DB (2009) “Hypersonic Vehicle Thrust Sensitivity to Angle of Attack and Mach Number. In: AIAA Atmospheric Flight Mechanics Conference, AIAA Paper 2009-6152. https://doi.org/10.2514/6.2009-6152
3. Torrez SM, Driscoll JF, Dalle DJ, Fotia ML (2009) Preliminary Design Methodology for Hypersonic Engine flow paths. In: 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, AIAA Paper 2009-7289. https://doi.org/10.2514/6.2009-7289
4. Vedam AJ, Devaraj MKK, Jagadeesh G (2019) Limitations of Two-Shock Mixed Compression Intakes at Hypersonic Mach Numbers. In: Conference AIAA Aviation Forum. https://doi.org/10.2514/6.2019-3592
5. Dalle DJ, Torrezy SM, Driscollz JF (2011) Performance Analysis of Variable-Geometry Scramjet Inlets Using a Low-Order Model. In: 47thAIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 31 July–03 August, San Diego, California. https://doi.org/10.2514/6.2011-5756
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