Statistical analysis and multiple regression were used to determine and quantify the significant hygrothermomechanical variables which infuence the tensile durability/life (cycle loading, fatigue) of boron-fiber/epoxy-matrix (B/E) and high-modulus-fiber/epoxy-matrix (HMS/E) composites. The use of the multiple regression analysis reduced the variables from fifteen, assumed initially, to six or less with a probability of greater than 0.999. The reduced variables were used to derive predictive models for compression an intralaminar shear durability/life of B/E and HMS/E composites assuming isoparametric fatigue behavior. The predictive models were subsequently generalized to predict the durability/life of graphite-fiber-r generalized model is ...
Hygrothermomechanical fracture stress criteria are developed and evaluated for unidirectional compos...
Fiber reinforced polymer composites offer significant advantages over traditional structural materia...
A prerequisite for full utilization of composite materials in aerospace components is accurate desig...
Technological solutions that will ensure the economic viability and environmental compatibility of a...
A methodology to compute probabilistic fatigue life of polymer matrix laminated composites has been ...
Advanced mechanical and structural applications require accurate assessment and better knowledge of ...
The static and cyclic load behavior of transverse filament tape (TFT) fiberglass/epoxy and TFY fiber...
The use of composite materials in U.S. Navy aircraft and other vessels has become increasingly popul...
The influence of hygrothermal environmental conditions on the load carrying ability and response of ...
Although being a crucial step in structural design of laminated composites, prediction of their long...
The work done in this investigation is part of a continuing program designed to develop probabilist...
An engineering approach to predict the fatigue life and progressive failure of multilayered composit...
A convenient procedure is described to determine the hygral behavior (moisture expansion coefficient...
The fatigue behavior of multidirectional graphite-epoxy laminates was analyzed theoretically and exp...
A strain-based fatigue life prediction method is proposed for an intermetallic matrix composite (IMC...
Hygrothermomechanical fracture stress criteria are developed and evaluated for unidirectional compos...
Fiber reinforced polymer composites offer significant advantages over traditional structural materia...
A prerequisite for full utilization of composite materials in aerospace components is accurate desig...
Technological solutions that will ensure the economic viability and environmental compatibility of a...
A methodology to compute probabilistic fatigue life of polymer matrix laminated composites has been ...
Advanced mechanical and structural applications require accurate assessment and better knowledge of ...
The static and cyclic load behavior of transverse filament tape (TFT) fiberglass/epoxy and TFY fiber...
The use of composite materials in U.S. Navy aircraft and other vessels has become increasingly popul...
The influence of hygrothermal environmental conditions on the load carrying ability and response of ...
Although being a crucial step in structural design of laminated composites, prediction of their long...
The work done in this investigation is part of a continuing program designed to develop probabilist...
An engineering approach to predict the fatigue life and progressive failure of multilayered composit...
A convenient procedure is described to determine the hygral behavior (moisture expansion coefficient...
The fatigue behavior of multidirectional graphite-epoxy laminates was analyzed theoretically and exp...
A strain-based fatigue life prediction method is proposed for an intermetallic matrix composite (IMC...
Hygrothermomechanical fracture stress criteria are developed and evaluated for unidirectional compos...
Fiber reinforced polymer composites offer significant advantages over traditional structural materia...
A prerequisite for full utilization of composite materials in aerospace components is accurate desig...