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You searched for subject:(stitch bonded). Showing records 1 – 2 of 2 total matches.

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Virginia Tech

1. Vandermey, Nancy E. Damage development under compression-compression fatigue loading in a stitched uniwoven graphite/epoxy composite material.

Degree: MS, Engineering Mechanics, 1991, Virginia Tech

Damage initiation and growth under compression-compression fatigue loading were investigated for a stitched uniweave material system with an underlying AS4/3501-6 quasi-isotropic layup. Performance of unnotched specimens having stitch rows at either 0° or 90° to the loading direction was compared. Special attention was given to the effects of stitching-related manufacturing defects. Damage evaluation techniques included edge replication, stiffness monitoring, X-ray radiography, residual compressive strength, and laminate sectioning. It was found that the manufacturing defect of inclined stitches had the greatest adverse effect on material performance. 0° and 90° specimen performances were generally the same. While the stitches were the source of damage initiation, they also slowed damage propagation both along the length and across the width and affected through the thickness damage growth. A pinched layer zone formed by the stitches particularly affected damage initiation and growth. The compression failure mode was transverse shear for all specimens, both in static compression and fatigue cycling tests. Specimens without stitches were not available for comparison.

Subjects/Keywords: Stitch-bonded fabrics.; LD5655.V855 1991.V367

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Vandermey, N. E. (1991). Damage development under compression-compression fatigue loading in a stitched uniwoven graphite/epoxy composite material. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/45318

Chicago Manual of Style (16th Edition):

Vandermey, Nancy E. “Damage development under compression-compression fatigue loading in a stitched uniwoven graphite/epoxy composite material.” 1991. Masters Thesis, Virginia Tech. Accessed March 05, 2021. http://hdl.handle.net/10919/45318.

MLA Handbook (7th Edition):

Vandermey, Nancy E. “Damage development under compression-compression fatigue loading in a stitched uniwoven graphite/epoxy composite material.” 1991. Web. 05 Mar 2021.

Vancouver:

Vandermey NE. Damage development under compression-compression fatigue loading in a stitched uniwoven graphite/epoxy composite material. [Internet] [Masters thesis]. Virginia Tech; 1991. [cited 2021 Mar 05]. Available from: http://hdl.handle.net/10919/45318.

Council of Science Editors:

Vandermey NE. Damage development under compression-compression fatigue loading in a stitched uniwoven graphite/epoxy composite material. [Masters Thesis]. Virginia Tech; 1991. Available from: http://hdl.handle.net/10919/45318


Penn State University

2. Haluza, Rudy T. Mechanical Response of Out-Of-Autoclave Complex Fiber Architecture Composites for Marine Structures.

Degree: 2017, Penn State University

Hydrokinetic turbines have shown promise as a novel method for harvesting power from natural waterways. The customizability of these turbines allows for smaller turbine systems compared to large, geographically demanding hydroelectric plants. However, maintenance costs stemming from relatively short service lives of existing glass/epoxy turbine blades impede the growth of hydrokinetic power. In prototype blades, fatigue loading in salt water caused relatively rapid degradation and subsequent high maintenance costs. Thus, fatigue-resistant blades designed for multi-decade service life would lower the net cost of hydrokinetic turbine usage and increase the feasibility, and therefore growth, of hydrokinetic turbine usage. Furthermore, material systems chosen for hydrokinetic blade use must be studied in order to understand their behavior in long-term under-sea conditions. This study researched the tensile-mechanical response of a quasi-isotropic woven and stitched laminate under quasi-static and fatigue loading at a stress ratio (R) of 0.1 and a frequency of 10 Hz. Some fatigue samples were fatigued until failure, while others underwent residual modulus and strength measurements. Both woven and stitched laminates were found to survive ten million cycles with a maximum stress of +13.75 ksi, but fail prior to ten-million cycles with a maximum stress of +18 ksi. In room-temperature ambient conditions, the polyester-stitched composite proved to have superior fatigue life only in long-life (>105 cycles) fatigue tests. Damaged, but not failed samples showed similar trends in that stitched samples would have more damage at lower cycle counts, but less damage at higher cycle counts compared to woven samples. However, there was more statistical scatter within the stitched specimens compared to woven specimens. Samples that were conditioned and tested while submerged in water had 30% reduction in tensile strength compared to the non-conditioned samples tested in ambient conditions. The partially saturated samples also showed damage accumulation and failure occurring nearly a decade earlier than the non-conditioned samples. Through optical macroscopic and microscopic investigation, intralaminar cracks and delaminations were found to occur in damaged woven samples, while stitched samples showed higher densities of unconnected intralaminar cracks before failure. Delaminations were found in near-failure stitch-bonded samples, especially in those tested at higher maximum fatigue stresses. More intralaminar cracks were found within stitched specimens compared to woven specimens that had similar reductions in elastic modulus, although, stitched specimens showed greater strength retention compared to the woven specimens. Future research could utilize these macroscopic and microscopic crack densities to develop models to better predict turbine blade damage at given loading levels and cycles. Advisors/Committee Members: Kevin L Koudela, Thesis Advisor/Co-Advisor.

Subjects/Keywords: hydro; kinetic; turbine; hydrokinetic; composite; glass; fiber; epoxy; water; marine; fatigue; tension; ooa; out-of-autoclave; damage; fail; condtioning; elevated; temperature; seawater; absorption; model; quasi-laminar; quasi-static; 0.1; tension-tension; sun-li; modulus; residual; strength; reduction; VARTM; woven; weave; stitch; stitch-bonded; textile; wet

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Haluza, R. T. (2017). Mechanical Response of Out-Of-Autoclave Complex Fiber Architecture Composites for Marine Structures. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/14482rth5095

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Haluza, Rudy T. “Mechanical Response of Out-Of-Autoclave Complex Fiber Architecture Composites for Marine Structures.” 2017. Thesis, Penn State University. Accessed March 05, 2021. https://submit-etda.libraries.psu.edu/catalog/14482rth5095.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Haluza, Rudy T. “Mechanical Response of Out-Of-Autoclave Complex Fiber Architecture Composites for Marine Structures.” 2017. Web. 05 Mar 2021.

Vancouver:

Haluza RT. Mechanical Response of Out-Of-Autoclave Complex Fiber Architecture Composites for Marine Structures. [Internet] [Thesis]. Penn State University; 2017. [cited 2021 Mar 05]. Available from: https://submit-etda.libraries.psu.edu/catalog/14482rth5095.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Haluza RT. Mechanical Response of Out-Of-Autoclave Complex Fiber Architecture Composites for Marine Structures. [Thesis]. Penn State University; 2017. Available from: https://submit-etda.libraries.psu.edu/catalog/14482rth5095

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

.