Fatigue Crack Growth Properties of a GLARE3-5/4 Fiber/Metal Laminate

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概要

• 論文の詳細を見る
• 宇宙航空研究開発機構の論文

著者

• SHIMOKAWA Toshiyuki

  National Aerospace Laboratory

• KAKUTA Yoshiaki

  National Aerospace Laboratory

• TAKAMATSU Toru

  University of Electro-Communications

• MATSUMURA Takashi

  University of Electro-Communications

• OGURA Norio

  Matsushita Communication Industrial

関連論文

• 2母数ワイブル分布における最良母数推定法の選択 : 材料強度分布の母数定数に関連して
• Fatigue Crack Propagation of Some Aircraft Sheet Materials (the Transactions of the Japan Society of Mechanical Engineers) : Papers published in the Bulletin of the JSME are not included here
• Goodness-of-Fit Tests for the Type-I Extreme-Value and Two-Parameter Weibull Distributions with Unknown Parameters Estimated by Graphical Plotting Techniques ------ Part 1:Critical Values
• A Statistical Consideration of S-N Tests (Specimen Allocation to the Inclined and Horizontal Parts of the S-N curve)
• Goodness-of-Fit Tests for the Type-I Extreme-Value and Two-Parameter Weibull Distributions with Unknown Parameters Estimated by Graphical Plotting Techniques ------ Part 2:Power Study
• Fatigue Crack Growth Properties of a GLARE3-5/4 Fiber/Metal Laminate

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