書誌事項
- タイトル別名
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- Non-Linear Free Flexural Vibration of Heated Plates With Initial Deflection
抄録
The problems of thermal stress and vibration of structural components and structures, resulting from the aerodynamic heating encountered in the supersonic flight and from the extremely high temperature induced in combustion chambers and exhaust pipes, have been of great importance in connection with the development of missiles and artificial satellites. <BR>In the present paper, the fundamental equations of non-linear free flexural vibration for a heated rectangular plate, taking the initial deflection into account, are solved approximately by employing a method of successive approximation, and the influences of the initial deflection, temperature change and large amplitude on the period of free vibration are established. <BR>Then, some experimental results on the free vibration of a plate subjected to the change in temperature are presented. It is shown that the experimental results agree qualitatively with the theoretical one.
収録刊行物
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- 日本航空学会誌
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日本航空学会誌 15 (157), 39-46, 1967
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390282680347855744
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- NII論文ID
- 130003781922
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- ISSN
- 24323039
- 18835422
- 00214663
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可