Reference health
Damage-tolerant composite design principles for aircraft components under fatigue service loading using multi-scale progressive failure analysis
44/44 checkable references clean · checked 2026-08-10
Every reference with a DOI in the deposited reference list resolved to a known work in Crossref or DataCite at the dated check, and none carried a retraction, withdrawal, or removal notice.
13 without a DOI — not checked. A reference deposited without a DOI is never matched by title or guessed at; it stays outside the checked set, and this line discloses that.
The 44 checked references that resolve
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Fatigue Validation of Composite Open Hole Analysis Technique for Standard and Nonstandard Laminate - Part 2
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Fatigue Failure Model for Fibre-Reinforced Materials under General Loading Conditions
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Life prediction for fatigue of T800/5245 carbob-fibre composites: II. Variable-amplitude loading
resolves10.1177/002199839402801305
Loading Rate and Temperature Dependence on Flexural Fatigue Behavior of a Satin Woven CFRP Laminate
resolves10.1016/S0263-8223(00)00092-1
Experimental set-up for and numerical modelling of bending fatigue experiments on plain woven glass/epoxy composites
resolves10.1177/002199838702100405
Modeling Stiffness Reduction of Graphite/Epoxy Composite Laminates
resolves10.1016/S0263-8223(97)00142-6
A stiffness degradation model for composite laminates under fatigue loading
resolves10.1520/STP36922S
Degradation and Sudden-Death Models of Fatigue of Graphite/Epoxy Composites
resolves10.1177/0021998308104357
Fatigue Model for Composites Based on the Cycle-by-cycle Probability of Failure: Implications and Applications
resolves10.1177/0021998307078735
Fatigue Life Prediction of Composite Structures Under Constant Amplitude Loading
resolves10.1002/nme.1620270208
Fatigue life estimation of graphite/epoxy laminates under consideration of delamination growth
resolves10.1016/0013-7944(86)90038-X
Stiffness properties of composite laminates with matrix cracking and interior delamination
resolves10.1177/002199839202601105
Transverse Cracking and Stiffness Reduction in Cross Ply Laminates of Different Matrix Toughness
resolves10.1177/0021998313499478
Micromechanics-based progressive failure analysis prediction for WWFE-III composite coupon test cases
resolves10.1016/0266-3538(93)90040-N
In-situ damage evolution and micro/macro transition for laminated composites
resolves10.1016/0010-4361(92)90327-Q
Analysis of multiple matrix cracking in [±θm/90n]s composite laminates. Part 1: In-plane stiffness properties
resolves10.1016/0010-4361(92)90328-R
Analysis of multiple matrix cracking in [±θm/90n]s composite laminates. Part 2: Development of transverse ply cracks
resolves10.2514/6.2007-2381
Estimation of Fatigue and Fracture Allowables For Metallic Materials Under Cyclic Loading
resolves10.1016/j.finel.2006.03.007
Progressive crack growth analysis using interface element based on the virtual crack closure technique
resolves10.2514/6.2015-1878
Static Validation of Composite Open Hole Analysis Technique for Standard and nonstandard Laminate -Part 1
resolves10.2514/6.2005-2226
Prediction of Micro-Crack Densities in IM7/977-2 Polymer Composite Laminates Under Mechanical Loading at Room and Cryogenic Temperatures
resolves10.4271/2006-01-0001
A Math-Based Methodology for Fatigue Longevity Prediction of 3D Woven Fiberglass Reinforced Vinyl-ester Composites
resolves10.4271/2008-01-0541
Technical Approach for Coupled Reliability-Durability Assessment of Army Vehicle Sub-Assemblies
resolves10.1016/j.compstruc.2011.01.021
Collision provoked failure sequencing in space reentry vehicles
The 13 references without a DOI — listed, not checked
no DOI — not checkedLMA/AFRL Journal Publication Fatigue, 2016.
no DOI — not checkedKawai M. Damage mechanics model for off-axis fatigue behavior of unidirectional carbon fiber-reinforced composites at room and high temperatures. In:
Proceedings of 12th international conference on composite materials (ICCM-12)
. Paris, France, 5–9 July 1999, p.322.
no DOI — not checkedPredicting the structural performance of composite structures under cyclic loading
no DOI — not checkedMurthy PLN and Chamis CC. Integrated Composite Analyzer (ICAN): Users and programmers manual. NASA Technical Paper, 1986.
no DOI — not checkedFarahmand B, Bockrath G and Glassco J.
Fatigue and Fracture Mechanics of High Risk Parts: Application of LEFM and FMDM Theory
. Springer Science and Business Media, 2012.
no DOI — not checkedFracture mechanics of metals, composites, welds, and bolted joints: application of LEFM, EPFM, and FMDM theory
no DOI — not checkedFarahmand B and Abdi F. Probabilistic fracture toughness, fatigue crack growth estimation resulting from material uncertainties. ASTM international Paper, 11569, 2002, pp.6-7.
no DOI — not checkedASC JCM, Static, 2016.
no DOI — not checkedLi Q, Minnetyan L and Chamis CC. Structural durability and fatigue of composites in acoustic environment.
SAMPE Conference Paper
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no DOI — not checkedTech Scout 1 final review (Air Force Research Lab): assess and quantify the benefits of applying damage tolerant design principles (DTDP) to advanced composite aircraft structures
no DOI — not checkedMCQ Composites 1.7 user’s manual, 2015.
no DOI — not checkedSchoeppner G and Clay S. Challenges associated with integrating composites into air force applications.
AF Life Cycle Management Center Presentation at Composite Materials and Computational Tools Workshop: Industrial, Academic, and Government Perspective to DOD Applications
, Wright-Patterson Air Force Base, Ohio, USA, 4–5 November 2014.
no DOI — not checkedTech Scout 1 Final review (Lockheed Martin): assess and quantify the benefits of applying damage tolerant design principles (DTDP) to advanced composite aircraft structures
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