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Dynamic Ensemble Learning with Transfer Learning for Fatigue Performance Prediction in Ni-Based Superalloys. [PDF]
Materials (Basel)Yang J, Du F, Lv H, Li W, Wu D.
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Fatigue Failure Mechanism and Crack Growth Behavior of Ti-6Al-4V ELI Titanium Alloy Welded Joints. [PDF]
Materials (Basel)Liu J, Li Y, Rui SS, Chen W, Sun C.
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Effects of the Intensity, Duration, and Muscle Mass of Isometric Handgrip Exercise on Neuromuscular Fatigue and Post-Exercise Blood Pressure Responses: A Crossover Study. [PDF]
Health Sci RepWang J +4 more
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Herbal and pharmacological treatments in cancer-related fatigue. [PDF]
Transl Gastroenterol HepatolFukuda K, Hamada T, Takeda T.
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, 1997 This volume contains a selection of papers presented at Fatigue Design 95 held in Helsinki, Finland from 5-8 September 1995. The papers have been peer reviewed and present practical aspects for the design of components and structures to avoid fatigue ...
International Symposium on Fatigue Design < 1995, Helsinki, Finland> +4 more
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Fatigue and the Design of the Respiratory System
1995One source of muscle fatigue may be the failure to provide the required oxygen by any step in the oxygen transport cascade or a lack of the necessary machinery to utilize that oxygen. We favor abandoning the concept of a single rate-limiting step for the concept of tuned resistors, each contributing to the overall resistance to oxygen flow.
S L, Lindstedt, H, Hoppeler
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Minerals Engineering, 2012
Abstract Strain-gauge measurements from a large ball mill are presented. Stress ranges determined from these strain-gauge measurements are compared with calculated stress ranges from a finite element analysis of the mill. It is shown that liner stiffness effects can result in lower-than-expected stress ranges at inboard plate flanges in the mill ...
C. Meimaris, W.K.K. Lai
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Abstract Strain-gauge measurements from a large ball mill are presented. Stress ranges determined from these strain-gauge measurements are compared with calculated stress ranges from a finite element analysis of the mill. It is shown that liner stiffness effects can result in lower-than-expected stress ranges at inboard plate flanges in the mill ...
C. Meimaris, W.K.K. Lai
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SAE Technical Paper Series, 1954
<div class="section abstract"><div class="htmlview paragraph">STEPS in fatigue design of aircraft lower wing surfaces, as presented here, are: <ol class="list nostyle"> <li class="list-item"> <span class="li-label">1.</span> <div class="htmlview ...
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<div class="section abstract"><div class="htmlview paragraph">STEPS in fatigue design of aircraft lower wing surfaces, as presented here, are: <ol class="list nostyle"> <li class="list-item"> <span class="li-label">1.</span> <div class="htmlview ...
openaire +1 more source