2017
DOI: 10.1007/978-3-642-55248-9
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Load Assumption for Fatigue Design of Structures and Components

Abstract: the material is concerned, specifically the rights of translation, reprinting, reuse of illustrations, recitation, broadcasting, reproduction on microfilms or in any other physical way, and transmission or information storage and retrieval, electronic adaptation, computer software, or by similar or dissimilar methodology now known or hereafter developed. The use of general descriptive names, registered names, trademarks, service marks, etc. in this publication does not imply, even in the absence of a specific … Show more

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Cited by 17 publications
(11 citation statements)
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“…Background information and further details on the method used to generate the random load sequence can be found in [33][34][35][36][37][38][39][40][41][42][43][44][45][46][47][48][49][50] and will be described and discussed in detail in the near future. This section describes the testing procedure and the realization of the different load sequences of a p (1/3) spectrum in relation to the sequence effect.…”
Section: Load Sequences and Testing Proceduresmentioning
confidence: 99%
“…Background information and further details on the method used to generate the random load sequence can be found in [33][34][35][36][37][38][39][40][41][42][43][44][45][46][47][48][49][50] and will be described and discussed in detail in the near future. This section describes the testing procedure and the realization of the different load sequences of a p (1/3) spectrum in relation to the sequence effect.…”
Section: Load Sequences and Testing Proceduresmentioning
confidence: 99%
“…The case of components subjected to multiple inputs of loads is considered as difficult (see [12], Chapter 6), even in the simple case where the linear superposition principle holds, because of the unknown interactions of the different loads at the local scale. Industrial practice is not well documented but to our knowledge usually consists in analyzing each channel independently.…”
Section: Elastic Quasi-static Nd Loadmentioning
confidence: 99%
“…Find p * eq such as ∀p, D • L(F eq (p * eq ), p) = D • L(F, p) (12) with p the parameters for any points of any structure in the scope of the design possibilities. Unfortunately this condition is almost never satisfied.…”
Section: Strong Formulation Of the Damage Equivalence Conditionmentioning
confidence: 99%
“…Bu çalışmalarda ortaya koyulan temel olgular günümüzde de yapılan çalışmaların temelini oluşturmaktadır. (Köhler, Jenne, Pötter, & Zenner, 2017;Marczewska et al, 2006). Malzemelerin ve makine parçalarının yorulma davranışları yorulma ömür (S-N) eğrileri ile belirlenmektedir (Toasa Caiza & Ummenhofer, 2018).…”
Section: Introductionunclassified