Kodama Shotaro | Faculty Of Technology Tokyo Metropolitan Univ.
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概要
関連著者
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Kodama Shotaro
Faculty Of Technology Tokyo Metropolitan Univ.
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KODAMA Shotaro
Faculty of Technology, Tokyo Metropolitan Univ.
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Kodama Shotaro
Faculty Of Technology Tokyo Metropolitan University
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Fujii Hajime
Faculty Of Engineering Chiba University
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SATO Kenkichi
Faculty of Engineering, Chiba University
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Misawa Hiroshi
Faculty Of Technology Tokyo Metropolitan University
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Misawa Hiroshi
Faculty Of Engineering Tokyo Metropolitan University
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Sato Kenkichi
Faculty Of Engineering Chiba University
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MISAWA Hiroshi
Faculty of Technology, Tokyo Metropolitan University
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FUKUSHIMA Akira
Faculty of Engineering, Yamanashi Univ.
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KAWAKAMI Yoshimichi
Mitsubishi Heavy Industries, Ltd., Yokohama Technical Institute
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Fukushima Akira
Faculty Of Engineering Yamanashi Univ.
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Kawakami Yoshimichi
Mitsubishi Heavy Industries Ltd. Yokohama Technical Institute
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Kawada Yuichi
Tokyo Metropolitan University
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Kawada Yuichi
Tokyo Metropolitan College Of Engineering
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Tsuchida Koji
Faculty Of Technology Tokyo Metropolitan Univ.
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HAREYAMA Soichi
Technical Research Laboratory, Toyo Umpanki Co.,Ltd.
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KAWAKAMI Yoshimichi
Faculty of Technology, Tokyo Metropolitan University
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Hareyama Soichi
Technical Research Laboratory Toyo Umpanki Co. Ltd.
著作論文
- A Study on the Residual Stress Distributions by Turning
- Stress Intensity Factors for Fretting Fatigue Cracks and Representation of Cracks Propagation Behavior Using the Stress Intensity Factors : Series A : Solid-Mechanics, Strength of Materials
- Effects of Stress Ratio and Fretting Fatigue Cycles on the Accumulation of Fretting Fatigue Damage of Carbon Steel S 45 C
- Crack Propagation Behavior in Fretting Fatigue of S45C Carbon Steel
- A Study on the Contidence Limit for Two Independent Probability Variables in Engineering Problems : Applications to Limit of Transmitted Torque in Disk Clutch and Bolt Axial Tension Control
- A ΔK_th Testing Method based on the Plastic Zone Slze at the Fatigue Crack Tip
- Fatigue Crack Propagation Behavior in 2024-T 3 Aluminium Alloys under Simplified Flight-Simulation Loading : Series A : Solid-Mechanics, Strength of Materials
- Effect of a Very Small Number of Stress Cycles above Fatigue Limit on Crack Propagation Behavior under Variable Stress Amplitude