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Effect of Initial Position of Tornado-driven Missiles on Dispersion Features
Bibliographic Information
- Other Title
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- 竜巻飛来物飛散特性に対する物体初期位置の影響評価
Description
Liftoff and flight behaviors of tornado missiles, which are initially placed on the ground, are computed using the Fujita's DBT-77 model. The results have revealed the dependency on the initial positions and the cumulative probability distribution of flight distance and maximum velocity. It is found the results of the U.S. NRC guide method, where a missile is released from a specific point at 40m elevation, correspond to more than 90% exceedance probabilities.
Journal
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- Summaries to Technical Papers of Annual Meeting, Japan Association for Wind Engineering
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Summaries to Technical Papers of Annual Meeting, Japan Association for Wind Engineering 2015 (0), 151-152, 2015
Japan Association for Wind Engineering
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Keywords
Details 詳細情報について
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- CRID
- 1390282680601848960
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- NII Article ID
- 130005485618
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- Text Lang
- ja
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- Data Source
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- JaLC
- CiNii Articles
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- Abstract License Flag
- Disallowed