Probabilistic damage tolerance assessment method based on the multi-scale crack growth model-Reference-Cited by-同舟云学术

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Probabilistic damage tolerance assessment method based on the multi-scale crack growth model

Published:2023-06 Issue: Volume:285 Page:109297
ISSN:0013-7944
Container-title:Engineering Fracture Mechanics
language:en
Short-container-title:Engineering Fracture Mechanics

Author:

Lu Rong-Sheng,Yang Jie^ORCID,Wang Ji,Wang Run-Zi,Shlyannikov Valery,Zhang Xian-Cheng,Tu Shan-Tung

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference41 articles.

1. Comprehensive structural integrity: Cyclic loading and fatigue;Milne,2003

2. Manning S, Garver W, Henslee S, Norris J, Pendley B. Durability Methods Development. Volume 1-Phase 1-Summary. GENERAL DYNAMICS FORT WORTH TX FORT WORTH DIV; 1979.

3. Department of Defense Standard Practice: Aircraft Structural Integrity Program (ASIP);Defense;MIL-STD-1530D,2016

4. MIL-A-83444—Airplane Damage Tolerance Requirements;Specification;USAF,1974

5. Stan D. STAN 00-970. Design and Airworthiness Requirement for Service Aircraft. 1999.

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1. Fatigue crack damage tolerance life prediction based on SCN-IHDMR method;International Journal of Fatigue;2024-01

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