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LOAD INTERACTION EFFECTS ON FATIGUE CRACK GROWTH IN TI-6A1-4V ALLOY

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Main Author: NASA, WASHINGTON DC, APRIL 1973
Format: NASA-CR Book
Terbitan: NULL
Online Access: http://kinerja.lib.itb.ac.id/ftmd/index.php/bibliografi/detail/3168
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Lihat Juga

  • Effects of Load Spectrum Variations on Fatigue Crack Growth in 2024 T-3 Alumunium Alloy Sheet Material Under Flight Simulation Loading Related to the CN-235 Aircraft
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    oleh: NASA, WASHINGTON DC, OCTOBER 1973
  • Influence of Maximum Fatigue Load on Probabilistic Aspect of Fatigue Crack Propagation Life at Specified Grown Crack in Magnesium Alloys
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    Terbitan: (2017)
  • Effect Of Tib In Al-6%Si-2%Fe Alloys On Microstructure, Impact Strength and Fatigue Crack Growth
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