Fatigue Crack Propagation Behavior in 2024-T 3 Aluminium Alloys under Simplified Flight-Simulation Loading : Series A : Solid-Mechanics, Strength of Materials
スポンサーリンク
概要
著者
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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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Kodama Shotaro
Faculty Of Technology Tokyo Metropolitan Univ.
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KAWAKAMI Yoshimichi
Mitsubishi Heavy Industries, Ltd., Yokohama Technical Institute
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Kawakami Yoshimichi
Mitsubishi Heavy Industries Ltd. Yokohama Technical Institute
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MISAWA Hiroshi
Faculty of Technology, Tokyo Metropolitan University
関連論文
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- The Effect of Stress Amplitude below the Fatigue Limit on Cumulative Fatigue Lives in Perforated Round Specimens
- Effects of the Stress Amplitudes Below the Fatigue Limit on Fatigue Lives in the Cylindrical Specimens Having a V-shape Groove
- The Crack Propagation by the Stress Amplitude below the Fatigue Limit
- 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
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- 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