Sensitivity analysis of flowfield modeling parameters upon the flow structure and aerodynamics of an opposing jet over a hypersonic blunt body
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference61 articles.
1. Concept of non-ablative thermal protection system for hypersonic vehicles;Liu;AIAA J,2013
2. Gopalan J, Menezes V, Reddy K, Hashimoto T, Sun M, Takayama K. Hypersonic buzz phenomenon on the spiked blunt cones. Reston: AIAA; 2003. Report No.: AIAA-2003-0284.
3. Experimental investigations of hypersonic flow over highly blunted cones with aerospikes;Menezes;AIAA J,2003
4. Effectiveness of aerospike for drag reduction on a blunt cone in hypersonic flow;Kulkarni;J Spacecraft Rockets,2010
5. Experimental investigation on drag and heat flux reduction in supersonic/hypersonic flows: A survey;Wang;Acta Astronaut,2016
Cited by 17 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Ultrasonic peening-waterjet composite surface modification of 7075-T6 aluminum alloy for residual stress release and transformation mechanism;Journal of Alloys and Compounds;2024-10
2. Angle-of-attack characteristics of opposing jet for improving drag and heat reduction;Physics of Fluids;2024-07-01
3. Large eddy simulation study on drag reduction performance of array-based plasma synthetic jet actuators;Chinese Journal of Aeronautics;2024-06
4. Multi Parameters Control Mechanism on Drag and Heat Reduction of Opposing Jet;AIAA SCITECH 2024 Forum;2024-01-04
5. Analysis of Oil Capture Characteristic and Global Sensitivity of Radial Oil Scoops with Different Blade Radius Differences for High-Speed Bearings;2024
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