Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 346
Book Description
This study is directed at assessing the static compression and R = 10 compression fatigue properties of graphite epoxy composites with ply drop-off discontinuities under severe operating environments including room temperature dry and wet, -65 F wet, and 218 F dry and wet. In 30-ply (+/-45)5/016/904c laminates, two 0 deg plies or four 45 deg plies are dropped off symmetrically in the middle of the specimen. Static strengths and moduli of elasticity are unaffected by these discontinuities, however, some proportional limit and Poisson's ratio values are changed significantly. At 1.25x106 cycles of constant frequency fatigue the maximum endurance limit stress level is degraded significantly in all cases by the two 0 deg ply dropoffs, but for the four 45 deg ply dropoffs it is unaffected or increased significantly. Surviving specimens exhibit residual strength that varies directly with the maximum applied cyclic compressive stress up to a threshold level. Detail data tables and plots are included. Scanning electron microscopy observations of the failed specimen fracture surfaces combined with micromechanics/point stress analysis and the analysis of ply dropoff effects are also included. (MM).
The Effects of Discontinuities on Compression Fatigue Properties of Advanced Composites
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 346
Book Description
This study is directed at assessing the static compression and R = 10 compression fatigue properties of graphite epoxy composites with ply drop-off discontinuities under severe operating environments including room temperature dry and wet, -65 F wet, and 218 F dry and wet. In 30-ply (+/-45)5/016/904c laminates, two 0 deg plies or four 45 deg plies are dropped off symmetrically in the middle of the specimen. Static strengths and moduli of elasticity are unaffected by these discontinuities, however, some proportional limit and Poisson's ratio values are changed significantly. At 1.25x106 cycles of constant frequency fatigue the maximum endurance limit stress level is degraded significantly in all cases by the two 0 deg ply dropoffs, but for the four 45 deg ply dropoffs it is unaffected or increased significantly. Surviving specimens exhibit residual strength that varies directly with the maximum applied cyclic compressive stress up to a threshold level. Detail data tables and plots are included. Scanning electron microscopy observations of the failed specimen fracture surfaces combined with micromechanics/point stress analysis and the analysis of ply dropoff effects are also included. (MM).
Publisher:
ISBN:
Category :
Languages : en
Pages : 346
Book Description
This study is directed at assessing the static compression and R = 10 compression fatigue properties of graphite epoxy composites with ply drop-off discontinuities under severe operating environments including room temperature dry and wet, -65 F wet, and 218 F dry and wet. In 30-ply (+/-45)5/016/904c laminates, two 0 deg plies or four 45 deg plies are dropped off symmetrically in the middle of the specimen. Static strengths and moduli of elasticity are unaffected by these discontinuities, however, some proportional limit and Poisson's ratio values are changed significantly. At 1.25x106 cycles of constant frequency fatigue the maximum endurance limit stress level is degraded significantly in all cases by the two 0 deg ply dropoffs, but for the four 45 deg ply dropoffs it is unaffected or increased significantly. Surviving specimens exhibit residual strength that varies directly with the maximum applied cyclic compressive stress up to a threshold level. Detail data tables and plots are included. Scanning electron microscopy observations of the failed specimen fracture surfaces combined with micromechanics/point stress analysis and the analysis of ply dropoff effects are also included. (MM).
Composite Materials
Author: Isaac M. Daniel
Publisher: ASTM International
ISBN: 9780803106956
Category : Technology & Engineering
Languages : en
Pages : 608
Book Description
Publisher: ASTM International
ISBN: 9780803106956
Category : Technology & Engineering
Languages : en
Pages : 608
Book Description
Engineered Materials Handbook
Author: Theodore J. Reinhart
Publisher:
ISBN: 9780871702791
Category :
Languages : en
Pages : 1008
Book Description
Publisher:
ISBN: 9780871702791
Category :
Languages : en
Pages : 1008
Book Description
Investigation of the Relations Between Neat Resin and Advanced Composite Mechanical Properties. Volume 1: Results
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 270
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 270
Book Description
Stiffness Reductions During Tensile Fatigue Testing of Graphite/epoxy Angle-ply Laminates
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 186
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 186
Book Description
1981 Advances in Aerospace Structures and Materials
Author: American Society of Mechanical Engineers. Winter Annual Meeting
Publisher:
ISBN:
Category : Aerospace industries
Languages : en
Pages : 326
Book Description
Publisher:
ISBN:
Category : Aerospace industries
Languages : en
Pages : 326
Book Description
Effect of Compression on Fatigue Properties of a Quasi-Isotropic Graphite/Epoxy Composite
Author: JT. Ryder
Publisher:
ISBN:
Category : Composite materials
Languages : en
Pages : 24
Book Description
The effect of compressive loading on the fatigue properties of a quasi-isotropic graphite/epoxy composite is discussed. Tests were conducted using parallel-sided, unnotched T300/934 graphite/epoxy coupons cured at 177°C (350°F). Results are based on a large sample size (number of coupons tested at a particular test condition) which allowed a statistically significant evaluation of data scatter. All tests were conducted at room temperature. Fatigue tests were conducted at 10 Hz under constant-amplitude loading. Static tensile and compressive properties were obtained for coupons without prior fatigue damage. Tension-tension and tension-compression fatigue stress-life curves were qualitatively evaluated using a small sample set at each stress level. Three specific stress levels were chosen and the extent of data scatter defined for each type of fatigue loading. Additional coupons were subjected to the same amount of fatigue damage and half were tested for tensile residual strength degradation and half for compressive. Such residual strength tests were conducted at the same two fatigue maximum stress levels for both tension-tension and tension-compression fatigue. Data scatter was larger for static compression tests than for static tension tests. Static and fatigue failure modes were dissimilar. Compressive load excursions reduced fatigue life especially at lower stress levels. At stress levels where fatigue failures occurred, degradation in residual strength due to fatigue also occurred. Data analysis was performed using three-parameter Weibull asymptotic fits, which proved to be superior in predicting failure rates than two-parameter fits. The effect of sample size on descriptions of data scatter and accuracy of extrapolation is discussed.
Publisher:
ISBN:
Category : Composite materials
Languages : en
Pages : 24
Book Description
The effect of compressive loading on the fatigue properties of a quasi-isotropic graphite/epoxy composite is discussed. Tests were conducted using parallel-sided, unnotched T300/934 graphite/epoxy coupons cured at 177°C (350°F). Results are based on a large sample size (number of coupons tested at a particular test condition) which allowed a statistically significant evaluation of data scatter. All tests were conducted at room temperature. Fatigue tests were conducted at 10 Hz under constant-amplitude loading. Static tensile and compressive properties were obtained for coupons without prior fatigue damage. Tension-tension and tension-compression fatigue stress-life curves were qualitatively evaluated using a small sample set at each stress level. Three specific stress levels were chosen and the extent of data scatter defined for each type of fatigue loading. Additional coupons were subjected to the same amount of fatigue damage and half were tested for tensile residual strength degradation and half for compressive. Such residual strength tests were conducted at the same two fatigue maximum stress levels for both tension-tension and tension-compression fatigue. Data scatter was larger for static compression tests than for static tension tests. Static and fatigue failure modes were dissimilar. Compressive load excursions reduced fatigue life especially at lower stress levels. At stress levels where fatigue failures occurred, degradation in residual strength due to fatigue also occurred. Data analysis was performed using three-parameter Weibull asymptotic fits, which proved to be superior in predicting failure rates than two-parameter fits. The effect of sample size on descriptions of data scatter and accuracy of extrapolation is discussed.
Cyclic Deformation, Fracture, and Nondestructive Evaluation of Advanced Materials
Author: Michael R. Mitchell
Publisher: ASTM International
ISBN: 0803114443
Category : Ceramic materials
Languages : en
Pages : 345
Book Description
Publisher: ASTM International
ISBN: 0803114443
Category : Ceramic materials
Languages : en
Pages : 345
Book Description
Composite Materials
Author:
Publisher:
ISBN:
Category : Composite materials
Languages : en
Pages : 608
Book Description
Publisher:
ISBN:
Category : Composite materials
Languages : en
Pages : 608
Book Description
Mechanical Properties Testing of Candidate Polymer Matrix Materials for Use in High Performance Composites
Author: Richard S. Zimmerman
Publisher:
ISBN:
Category : Polymeric composites
Languages : en
Pages : 308
Book Description
Publisher:
ISBN:
Category : Polymeric composites
Languages : en
Pages : 308
Book Description