Art

J-GLOBAL ID：201602207346525763   Reference number：16A0209684

Effect of Nozzle Configuration on Takeoff Noise of a Hypersonic Transport

ノズル形態が極超音速航空機の離陸騒音に及ぼす影響

Author (7)： SANO NORIHISA (群馬大学大学院理工学専攻) ,  TANAKA KYOHEI (群馬大学大学院理工学専攻) ,  ARAKI MIKIYA (群馬大学大学院理工学専攻) ,  KOJIMA TAKAYUKI (群馬大学大学院理工学府知能機械創製部門) ,  TAGUCHI HIDEYUKI (宇宙航空研究開発機構航空技術部門) ,  GONZALEZ PALENCIA Juan C. (群馬大学大学院理工学府知能機械創製部門) ,  SHIGA SEIICHI (群馬大学大学院理工学府知能機械創製部門)
Material： 日本航空宇宙学会論文集  (Journal of the Japan Society for Aeronautical and Space Sciences)
Volume： 64  Issue： 1  Page： 27-34 (J-STAGE)  Publication year： 2016 
JST Material Number： L3565A  ISSN： 1344-6460  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： JAPANESE (JA)

Thesaurus term： *hypersonic aircraft ,  nozzle ,  *aircraft noise ,  noise(pollution) ,  *take-off ,  noise level ,  database design ,  morphology(form) ,  airport
Semi thesaurus term： jet noise ,  perceived noise level ,  database construction ,  nozzle dimension

JST classification (1)： Aircraft noise  (TE01020I)

Reference (30)：

• 1) Kojima, T., Kobayashi, H., Taguchi, H., Fukiba, K., Fujita, K., Hatta, H., Goto, K. and Aoki, T.: Design Study of Hypersonic Components for Precooled Turbojet Engine, 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, AIAA Paper 2008-2504, Dayton, OH, 2008.
• 2) Kobayashi, H., Sawai, S., Taguchi, H., Kojima, T., Fukiba, K., Fujita, K. and Sato, T.: Hypersonic Turbojet Engine Design of a Balloon-Based Flight Test Vehicle, 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, AIAA Paper 2008-2620, Dayton, OH, 2008.
• 3) Taguchi, H., Harada, K., Kobayashi, H., Kojima, T., Hongoh, M., Masaki, D., Sawai, S. and Maru, Y.: Firing Test of a Hypersonic Turbojet Engine Installed on a Flight Test Vehicle, 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, AIAA 2009-7311, Bremen, Germany, 2009.
• 4) Kojima, T., Kobayashi, H., Taguchi, H. and Goto, K.: Design and Fabrication of Variable Nozzle for Precooled Turbojet Engine, 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, AIAA Paper 2009-7312, Bremen, Germany, 2009.
• 5) Miyamoto, H., Matsuo, A., Kojima, T. and Taguchi, H.: Numerical Analysis of Rectangular Plug Nozzle Considering Practical Geometry and Flow Conditions, 45th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2007-0031, Reno, NV, 2007.

Terms in the title (4)： 形態 ,  超音速航空機 ,  離陸 ,  騒音