An Experimental Result on Buckling of Cylindrical Shells with a Reinforced Cut-Out under Axial Compression
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- YASUI Yoshiaki
- 東海大学工学部動力機械工学科
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- KASUYA Hirakazu
- 東海大学工学部動力機械工学科
Bibliographic Information
- Other Title
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- 開口部補強円筒殻の軸圧縮座屈に関する一実験結果
- カイコウブ ホキョウ エントウカク ノ ジク アッシュク ザクツ ニ カンスル
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Description
The experimental results on the buckling of thin cylindrical shells with a reinforced circular hole under axial compressive load are presented and discussed. The shell around a hole is reinforced by thickening the annular area. The variation of buckling load with the thickness or the radius of the reinforcing area is measured experimentally for both cases of central loading and eccentric loading.<BR>It is found that the reinforcement by thickening the wall thickness is more effective compared with by broading the reinforcing radius in order to recover the buckling value of monocoque cylindrical shell with a circular hole. The specimens of cylindrical shells and reinforcement materials used for these tests were made of Lumirror Polyester Sheet.
Journal
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- Aeronautical and Space Sciences Japan
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Aeronautical and Space Sciences Japan 30 (341), 364-368, 1982
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390001204505878272
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- NII Article ID
- 130003782538
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- NII Book ID
- AN00189072
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- ISSN
- 24241369
- 00214663
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- NDL BIB ID
- 2454486
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed