Noise Reduction of a Supersonic Jet Using Gas Injection from a Nozzle Wall
Author:
Affiliation:
1. Department of Mechanical Engineering, Gunma University
Publisher
Japan Society of Mechanical Engineers
Subject
Mechanical Engineering,Condensed Matter Physics
Link
http://www.jstage.jst.go.jp/article/kikaib1979/71/707/71_707_1798/_pdf
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. Prediction of Supersonic Jet Noise Radiated from Rectangular and Axi-Symmetric Plug Nozzles;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2009
2. Effects of Nozzle Scale, Total Temperature and an Afterburner on Jet Noise from a Pre-Cooled Turbojet Engine;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2009
3. Effects of Nozzle Geometry and Intermittent Injection of Aerodynamic Tab on Supersonic Jet Noise;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2008
4. Effects of Aerodynamic Tabs onExhaust Noise from a Rectangular Plug Nozzle;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2008
5. Effects of Aerodynamic Tabs on Screech Reduction of a Supersonic Jet;AIAA Journal;2006-02
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