Energy Addition–Based Virtual Cowl for Performance Enhancement of Scramjet Intake-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Energy Addition–Based Virtual Cowl for Performance Enhancement of Scramjet Intake

Published:2019-09 Issue:5 Volume:32 Page:04019076
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

John Bibin¹,Vijapuri Dhruv²,Thota Badriveer²,Katoch Neelesh²

Affiliation:

1. Associate Professor, School of Mechanical Engineering, Vellore Institute of Technology, Vellore, Tamil Nadu 632014, India (corresponding author).

2. Undergraduate Student, School of Mechanical Engineering, Vellore Institute of Technology, Vellore, Tamil Nadu 632014, India.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001067

Reference17 articles.

1. Bityurin V. A. A. I. Klimov and S. B. Leonov. 1999. “Assessment of a concept flow/flight control for hypersonic flights in atmosphere.” In Proc. 9th Int. Space Planes and Hypersonic Systems and Technologies Conf. 4820–4827. Reston VA: AIAA.

2. Concentrated energy addition for active drag reduction in hypersonic flow regime

3. Control of the Flow Past Bodies Using Localized Energy Addition to the Supersonic Oncoming Flow

4. Shock wave boundary layer interactions in hypersonic flows

Cited by 5 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. Rectangular-to-elliptical shape transition intakes with various leading-edge for performance enhancement;Acta Astronautica;2024-07

2. Investigation of pressure feedback technique to control ramp based SWBLI;Acta Astronautica;2022-12

3. Effect of isolator height on a model scramjet intake performance;Journal of Mechanical Science and Technology;2022-11-30

4. NUMERICAL STUDY OF RAMP-BASED SHOCK-INDUCED SEPARATION CONTROL IN HYPERSONIC FLOWS;International Journal of Fluid Mechanics Research;2022

5. Control of a Supersonic Inlet in Off-Design Conditions with Plasma Actuators and Bleed;Aerospace;2020-03-19

同舟云学术

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