Simple Jet Noise Reduction Technique for Variable Nozzle of Supersonic Aircraft-Reference-Cited by-同舟云学术

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Simple Jet Noise Reduction Technique for Variable Nozzle of Supersonic Aircraft

Published:2016-05-27 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA/CEAS Aeroacoustics Conference
language:
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Author:

Akatsuka Junichi¹,Watanabe Yasushi¹,Ishii Tatsuya¹

Affiliation:

1. Japan Aerospace Exploration Agency (JAXA)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-2988

Reference23 articles.

1. 1Wilhite,A.W.,Shaw,R.J."AnOverviewofNASA'sHigh-SpeedResearchProgram",20thICASCongress,2000.

2. 2Martin,S.,Mirzoyan,A."EnvironmentalProblemsoftheSSBJEngineintheHISACProject",ICASWorkshop2009.

3. 3Coen,P."SupersonicsProjectOverview",FundamentalAeronauticsProgramTechnicalConference2012.

Cited by 4 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. Comparative Study of Semi-empirical Jet Noise Prediction Models for Future Commercial Supersonic Aircraft;AIAA AVIATION 2021 FORUM;2021-07-28

2. System Noise Assessment of NASA Supersonic Technology Concept Aeroplane Using JAXA’s Noise Prediction Tool;AIAA Scitech 2020 Forum;2020-01-05

3. Experimental and Numerical Study of Jet Noise Reduction for Supersonic Aircraft Using Variable Folding Nozzle Concept;2018 AIAA/CEAS Aeroacoustics Conference;2018-06-24

4. Experimental Evaluation of Acoustic and Thrust Characteristics of Exhaust Nozzles using a Model Engine;AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2017

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