Effects of Nozzle Scale, Total Temperature and an Afterburner on Jet Noise from a Pre-Cooled Turbojet Engine-Reference-Cited by-同舟云学术

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Effects of Nozzle Scale, Total Temperature and an Afterburner on Jet Noise from a Pre-Cooled Turbojet Engine

Published:2009 Issue:663 Volume:57 Page:148-154
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,NISHIDA Shunsuke,IMAMURA Osamu,SHIGA Seiichi,TSUE Mitsuhiro

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/57/663/57_663_148/_pdf

Reference16 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. 2) 宇宙航空研究開発機構航空プログラムグループ極超音速機研究委員会: 極超音速機の研究開発構想,宇宙航空研究開発機構特別資料 JAXA-SP-06-025, 2007.

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

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

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

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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