000			03395nam a2200349 i 4500
008			080407s2009 paua b 001 0 eng d
020			_a9781932078862
020			_a193207886X
035			_a(OCoLC)221167095
040			_aBTCTA _cBTCTA _dBAKER _dYDXCP _dVPI
049			_aBAUN_MERKEZ
050	0	4	_aTA418.9.C6 _bH94 2009
100	1		_aHyer, M. W
245	1	0	_aStress analysis of fiber-reinforced composite materials / _cMichael W. Hyer ; contributions on fibers, matrices, interfaces, and manufacturing by Scott White
250			_aUpdated ed
264		1	_aLancaster, Pa. : _bDEStech Publications, Inc, _c[2009]
264		4	_c©2009
300			_axxii, 695 pages _billustrations ; _c24 cm
336			_atext _btxt _2rdacontent
337			_aunmediated _bn _2rdamedia
338			_avolume _bnc _2rdacarrier
520			_aUpdated and improved, Stress Analysis of Fiber-Reinforced Composite Materials, Hyer's work remains the definitive introduction to the use of mechanics to understand stresses in composites caused by deformations, loading, and temperature changes. In contrast to a materials science approach, Hyer emphasizes the micromechanics of stress and deformation for composite material analysis. The book provides invaluable analytic tools for students and engineers seeking to understand composite properties and failure limits. A key feature is a series of analytic problems continuing throughout the text, starting from relatively simple problems, which are built up step-by-step with accompanying calculations. The problem series uses the same material properties, so the impact of the elastic and thermal expansion properties for a single-layer of FR material on the stress, strains, elastic properties, thermal expansion and failure stress of cross-ply and angle-ply symmetric and unsymmetric laminates can be evaluated. The book shows how thermally induced stresses and strains due to curing, add to or subtract from those due to applied loads. Another important element, and one unique to this book, is an emphasis on the difference between specifying the applied loads, id est, force and moment results, often the case in practice, versus specifying strains and curvatures and determining the subsequent stresses and force and moment results. This represents a fundamental distinction in solid mechanics. - - Book Description
505	0	0	_t-- Fiber-reinforced composite materials _t-- Linear elastic stress-strain characteristics _t-- Prediction of engineering properties _t-- The plane-stress assumption _t-- Plane-stress stress-strain relations in a global coordinate system _t-- Classical lamination theory : the Kirchhoff hypothesis _t-- Classical lamination theory : laminate stiffness matrix _t-- Classical lamination theory : additional examples _t-- Failure theories for fiber-reinforced materials : maximum stress criterion _t-- Failure theories for fiber-reinforced materials : the Tsai-wu criterion _t-- Enviromentally induced stresses in laminates _t-- Through-thickness laminate strains _t-- Introduction to fiber-reinforced laminated plates _t-- Appendix : manufacturing composite laminates
504			_aIncludes bibliographical references and index
650		0	_aComposite materials
650		0	_aFibrous composites
650		0	_aLaminated materials
700	1		_aWhite, S. R. _q(Scott R.)
900			_a35399
900			_bsatın
942			_2lcc _cKT
999			_c32655 _d32655