Effects of Nozzle Geometry and Intermittent Injection of Aerodynamic Tab on Supersonic Jet Noise-Reference-Cited by-同舟云学术

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Effects of Nozzle Geometry and Intermittent Injection of Aerodynamic Tab on Supersonic Jet Noise

Published:2008 Issue:659 Volume:56 Page:590-595
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:ja
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

ARAKI Mikiya,SANO Takayuki,FUKUDA Masayuki,KOJIMA Takayuki,TAGUCHI Hideyuki,SHIGA Seiichi,OBOKATA Tomio

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/56/659/56_659_590/_pdf

Reference7 articles.

1. 1) Taguchi, H., Sato, T., Kobayashi, H., Kojima, T., Okai, K. and Fujita, K.: Design Study on a Small Pre-Cooled Turbojet Engine for Flight Experiments, AIAA Paper 2005-3419, 2005.

2. Noise Reduction of a Supersonic Jet Using Gas Injection from a Nozzle Wall

3. Effects of Aerodynamic Tabs on Screech Reduction of a Supersonic Jet

4. Noise Reduction Performance of Aerodynamic Tabs in a Supersonic Jet

5. Effects of Aerodynamic Tabs onExhaust Noise from a Rectangular Plug Nozzle

Cited by 1 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. Prediction of Supersonic Jet Noise Radiated from Rectangular and Axi-Symmetric Plug Nozzles;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2009

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