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Fatigue life prediction of GFRP comp...
~
Munagala, Praveenkumar.
Fatigue life prediction of GFRP composite material at coupon and component level.
紀錄類型:
書目-電子資源 : 單行本
正題名/作者:
Fatigue life prediction of GFRP composite material at coupon and component level./
作者:
Munagala, Praveenkumar.
面頁冊數:
112 p.
附註:
Source: Masters Abstracts International, Volume: 44-04, page: 1967.
Contained By:
Masters Abstracts International44-04.
標題:
Engineering, Mechanical. -
電子資源:
http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1431477
ISBN:
9780542477591
Fatigue life prediction of GFRP composite material at coupon and component level.
Munagala, Praveenkumar.
Fatigue life prediction of GFRP composite material at coupon and component level.
- 112 p.
Source: Masters Abstracts International, Volume: 44-04, page: 1967.
Thesis (M.S.M.E.)--West Virginia University, 2005.
In this study unidirectional, bidirectional glass fabric reinforced polymer (GFRP) composites were tested under fatigue loads to determine their fatigue life. The experimental fatigue life of FRP coupons was compared with the predicted fatigue life which was evaluated based on the internal strain energy model proposed by GangaRao and Natarajan (2003). It was found from the strain energy model that the power law accurately describes the relationship between energy release rate, DeltaU and normalized strain, x (applied strain to ultimate strain) as DeltaU = ax b, where 'a' and 'b' are the fatigue coefficients.
ISBN: 9780542477591Subjects--Topical Terms:
170925
Engineering, Mechanical.
Fatigue life prediction of GFRP composite material at coupon and component level.
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112 p.
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Source: Masters Abstracts International, Volume: 44-04, page: 1967.
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In this study unidirectional, bidirectional glass fabric reinforced polymer (GFRP) composites were tested under fatigue loads to determine their fatigue life. The experimental fatigue life of FRP coupons was compared with the predicted fatigue life which was evaluated based on the internal strain energy model proposed by GangaRao and Natarajan (2003). It was found from the strain energy model that the power law accurately describes the relationship between energy release rate, DeltaU and normalized strain, x (applied strain to ultimate strain) as DeltaU = ax b, where 'a' and 'b' are the fatigue coefficients.
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Further rectangular single cell and multi-cell GFRP deck components (Prodeck 4) were also evaluated under fatigue to determine their strain energy loss per cycle. It was found that the fatigue coefficient 'a' depends on the energy release rate while 'b' depends on material constants such as damping and bond strength between fibers/fabrics and matrix. (Abstract shortened by UMI.)
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