Combined Effects of External and Nozzle Exit Flows on the Jet Acoustic Power Levels of Chevron Nozzles for Transonic Aircraft

Author:

Ahmad Arsalan,Vinay Dekkala,Sundaria Shubhangi,Raza Sobia,Srivastasva Maansi,Singh Tanisha,Saha Sagnik,Kumar V. R. S.

Publisher

Springer Nature Singapore

Reference52 articles.

1. Ahmad A (2023) Design optimization of Chevron nozzle. AIAE NTCC-BTech-TR-AA-A3705519017, Undergraduate Project Report, Amity Institute of Aerospace Engineering, Amity University Uttar Pradesh, New Delhi NCR, India, May

2. Uzun A, Hussaini MY (2009) Simulation of noise generation in near-nozzle region of a Chevron nozzle jet. AIAA J 47:8. https://doi.org/10.2514/1.36659

3. Lyrintzis AS (2003) Surface integral methods in computational aeroacoustics: from the (CFD) near-field to the (acoustic) far field. Int J Aeroacoust 2(2):95–128

4. Sathyaprabha R, Vigneshwaran S, Manishaa R, Vivek S, Ajith S, Mani S, Kumar VRS (2016) Design of environmental friendly Chevron nozzles for lower stage rockets. In: 52nd AIAA/SAE/ASEE Joint Propulsion Conference, AIAA Propulsion and Energy Forum (AIAA 2016-4910). https://doi.org/10.2514/6.2016-4910

5. Sivabalan M, Lee DJ, Kumar VRS (2015) Jet acoustic characterization and geometrical optimization of Chevron nozzles using 3D k-ε model. In: 51st AIAA Joint Propulsion Conference, Florida, AIAA-2015-3884

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