| Project/Area Number |
26630442
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| Research Category |
Grant-in-Aid for Challenging Exploratory Research
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| Allocation Type | Multi-year Fund |
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| Research Field |
Aerospace engineering
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| Research Institution | Nagoya University |
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Principal Investigator |
SASOH Akihiro 名古屋大学, 工学(系)研究科(研究院), 教授 (40215752)
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| Co-Investigator(Renkei-kenkyūsha) |
YOKOTA Shigeru 筑波大学, システム情報系, 准教授 (30545778)
SAKAI Yasuhiko 名古屋大学, 大学院工学研究科, 教授 (20162274)
NAGATA Kouji 名古屋大学, 大学院工学研究科, 准教授 (50274501)
NAKAYAMA Yoshio 独立行政法人産業技術総合研究所, 安全科学研究部門, 研究グループ長 (20357677)
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| Project Period (FY) |
2014-04-01 – 2015-03-31
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| Project Status |
Completed (Fiscal Year 2014)
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| Budget Amount *help |
¥3,900,000 (Direct Cost: ¥3,000,000、Indirect Cost: ¥900,000)
Fiscal Year 2014: ¥3,900,000 (Direct Cost: ¥3,000,000、Indirect Cost: ¥900,000)
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| Keywords | 衝撃波 / ソニックブーム / 乱流 / 爆発実験 / 圧力変調 |
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| Outline of Final Research Achievements |
In this study, experimental simulation method of evaluating overpressure variation induced by a blast wave interacting with turbulent flow was developed. The blast wave was generated using a 0.51-gram power. The turbulent flow was generated with an electrical fan, duct and grid. Overpressure histories were measured using four microphones set symmetrically. A 40 % standard deviation in overpressure was obtained, thereby demonstrating spatiotemporal behavior as the result of the shock wave-turbulence interaction.
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