BIOMARKERS

Molecular Biopsy of Human Tumors

- a resource for Precision Medicine *

418 related articles for article (PubMed ID: 27242290)

  • 1. Modelling of stiffness degradation due to cracking in laminates subjected to multi-axial loading.
    Kashtalyan M; Soutis C
    Philos Trans A Math Phys Eng Sci; 2016 Jul; 374(2071):20160017. PubMed ID: 27242290
    [TBL] [Abstract][Full Text] [Related]  

  • 2. Prediction of failure in notched carbon-fibre-reinforced-polymer laminates under multi-axial loading.
    Tan JL; Deshpande VS; Fleck NA
    Philos Trans A Math Phys Eng Sci; 2016 Jul; 374(2071):20150273. PubMed ID: 27242302
    [TBL] [Abstract][Full Text] [Related]  

  • 3. Damage and failure modelling of hybrid three-dimensional textile composites: a mesh objective multi-scale approach.
    Patel DK; Waas AM
    Philos Trans A Math Phys Eng Sci; 2016 Jul; 374(2071):20160036. PubMed ID: 27242294
    [TBL] [Abstract][Full Text] [Related]  

  • 4. A Simplified Computational Strategy Focused on Resin Damage to Study Matrix Cracking of The Cross-Ply Laminates Under Uniaxial Tension Load.
    Sun L; Wang J; Hu H; Ni A
    Materials (Basel); 2019 Jun; 12(12):. PubMed ID: 31226770
    [TBL] [Abstract][Full Text] [Related]  

  • 5. Effect of ply orientation and through-thickness position of delamination on the reflection of fundamental symmetric S0 Lamb mode in GFRP composite plate structures.
    Gupta S; Rajagopal P
    Ultrasonics; 2018 Nov; 90():109-119. PubMed ID: 29940394
    [TBL] [Abstract][Full Text] [Related]  

  • 6. Acoustic emission monitoring of degradation of cross ply laminates.
    Aggelis DG; Barkoula NM; Matikas TE; Paipetis AS
    J Acoust Soc Am; 2010 Jun; 127(6):EL246-51. PubMed ID: 20550227
    [TBL] [Abstract][Full Text] [Related]  

  • 7. Fatigue Life Prediction for Transverse Crack Initiation of CFRP Cross-Ply and Quasi-Isotropic Laminates.
    Hosoi A; Kawada H
    Materials (Basel); 2018 Jul; 11(7):. PubMed ID: 29996529
    [TBL] [Abstract][Full Text] [Related]  

  • 8. Multi-axial damage and failure of medical grade carbon fibre reinforced PEEK laminates: Experimental testing and computational modelling.
    Gallagher EA; Lamorinière S; McGarry P
    J Mech Behav Biomed Mater; 2018 Jun; 82():154-167. PubMed ID: 29601987
    [TBL] [Abstract][Full Text] [Related]  

  • 9. Transverse Cracking Induced Acoustic Emission in Carbon Fiber-Epoxy Matrix Composite Laminates.
    Hamam Z; Godin N; Reynaud P; Fusco C; Carrère N; Doitrand A
    Materials (Basel); 2022 Jan; 15(1):. PubMed ID: 35009539
    [TBL] [Abstract][Full Text] [Related]  

  • 10. Hierarchical analysis of the degradation of fibre-reinforced polymers under the presence of void imperfections.
    Liebig WV; Schulte K; Fiedler B
    Philos Trans A Math Phys Eng Sci; 2016 Jul; 374(2071):20150279. PubMed ID: 27242296
    [TBL] [Abstract][Full Text] [Related]  

  • 11. Use of microfasteners to produce damage tolerant composite structures.
    Partridge IK; Hallett SR
    Philos Trans A Math Phys Eng Sci; 2016 Jul; 374(2071):20150277. PubMed ID: 27242299
    [TBL] [Abstract][Full Text] [Related]  

  • 12. Experimental Analysis of Matrix Cracking in Glass Fiber Reinforced Composite Off-Axis Plies under Static and Fatigue Loading.
    Just G; Koch I; Gude M
    Polymers (Basel); 2022 May; 14(11):. PubMed ID: 35683836
    [TBL] [Abstract][Full Text] [Related]  

  • 13. Relationship Between Matrix Cracking and Delamination in CFRP Cross-Ply Laminates Subjected to Low Velocity Impact.
    Tan R; Xu J; Sun W; Liu Z; Guan Z; Guo X
    Materials (Basel); 2019 Dec; 12(23):. PubMed ID: 31810160
    [TBL] [Abstract][Full Text] [Related]  

  • 14. The Influence of Ply Stacking Sequence on Mechanical Properties of Carbon/Epoxy Composite Laminates.
    Ogunleye RO; Rusnakova S; Zaludek M; Emebu S
    Polymers (Basel); 2022 Dec; 14(24):. PubMed ID: 36559933
    [TBL] [Abstract][Full Text] [Related]  

  • 15. Experimental and numerical investigations on the impact behaviour of pristine and patch-repaired composite laminates.
    Liu H; Brooks RA; Hall ZEC; Liu J; Crocker JWM; Joesbury AM; Harper LT; Blackman BRK; Kinloch AJ; Dear JP
    Philos Trans A Math Phys Eng Sci; 2022 Sep; 380(2232):20210340. PubMed ID: 35909361
    [TBL] [Abstract][Full Text] [Related]  

  • 16. A Fatigue Model to Predict Interlaminar Damage of FRP Composite Laminates Subjected to Mode I Load.
    Khan SA; Rahimian Koloor SS; King Jye W; Siebert G; Tamin MN
    Polymers (Basel); 2023 Jan; 15(3):. PubMed ID: 36771828
    [TBL] [Abstract][Full Text] [Related]  

  • 17. A comparison of different approaches for imaging cracks in composites by X-ray microtomography.
    Yu B; Bradley RS; Soutis C; Withers PJ
    Philos Trans A Math Phys Eng Sci; 2016 Jul; 374(2071):20160037. PubMed ID: 27242291
    [TBL] [Abstract][Full Text] [Related]  

  • 18. Numerical and Experimental Studies for Fatigue Damage Accumulation of CFRP Cross-Ply Laminates Based on Entropy Failure Criterion.
    Deng H; Mochizuki A; Fikry M; Abe S; Ogihara S; Koyanagi J
    Materials (Basel); 2022 Dec; 16(1):. PubMed ID: 36614726
    [TBL] [Abstract][Full Text] [Related]  

  • 19. Interlaminar Shear Strength and Failure Analysis of Aluminium-Carbon Laminates with a Glass Fiber Interlayer after Moisture Absorption.
    Bieniaś J; Jakubczak P; Droździel M; Surowska B
    Materials (Basel); 2020 Jul; 13(13):. PubMed ID: 32640550
    [TBL] [Abstract][Full Text] [Related]  

  • 20. J-Integral Experimental Reduction Reveals Fracture Toughness Improvements in Thin-Ply Carbon Fiber Laminates with Aligned Carbon Nanotube Interlaminar Reinforcement.
    Furtado C; Kopp R; Ni X; Sarrado C; Kalfon-Cohen E; Wardle BL; Camanho PP
    ACS Appl Mater Interfaces; 2024 Apr; 16(16):20980-9. PubMed ID: 38624137
    [TBL] [Abstract][Full Text] [Related]  

    [Next]    [New Search]
    of 21.