Mechanics Analysis Composite Materials Episode 1 doc

... 2.7 10 .7 4.5 33.3 1. 8 -1. 85 80.5 19 -19 .3 21. 1 10 .2 21. 5 1. 2 -1. 3 7.5 1. 2 -1. 35 5.8 1. 2 -1. 3 5.8 1. 35 -1. 4 3.7 1. 3 -1. 43 8.5 1. 2 6.7 0.95 4.7 1. 05 4.3 2.3 1. 5 1. 14 7.0 1. 32 4.5 1. 24 ... Chapter 1. Introduction 1 1. 1. Structural Materials 1 1. 2. Composite Materials 9 1. 2 .1. Fibers for Advanced Composites 10 1. 2.2. Matrix Mat...

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... 0.9 1 .o 1. 1 1. 15 I .o 12 .8 4.25 0.9 0.95 1 .o 1 .Q5 1. 1 1 .o 7.8 4.5 1 .o 1 .o 1 .o 1 .Q 1 .o 1 .o 0 5.0 Chapter 3. Mechanics ?fa unidirectional ply 61 The ... Bundle no. 1 2 3 4 5 0.6 0.7 0.85 0.9 0.95 0.8 0.9 0.9 0.85 0.95 1 .o 1. 2 1. 1 1 .o 0.95 1. 6 1. 4 1. 15 1. 05 0.95 3.0 I .6 1. 4 1. 1 0.95 *"...

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... 225 690 11 25 590 840 400 10 0 520 c:l 3 1. 43 1. 5 2.63 0.62 0.50 0.47 0.27 82 0. 31 0.45 0.75 0.2 0.37 0 .1 0.05 0 .13 El /E2 9.7 3.2 2 13 .1 1. 68 5 94 2 .1 18 6 Mechanics ... 4. Mechanics of u composite luyer 16 9 Total stresses in Eqs. (4 .1 10) and (4 .11 1) should satisfy equilibrium equations, Eqs. (2.5), which yield for the pro...

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... having diameter D = 1 m and total thickncss h = 13 .52 mm consists of four layers, i.e. = 0. 320 Mechanics and analysis of composite materials El 1. 5 1 0.5 ,% Q, = 600 ... (7. 41) Fig. 7 .17 . Creep diagram corresponding to mechanical model in Fig. 7 .16 . Fig. 7 .18 . Relaxation diagram corresponding to mechanical model in Fig. 7 .16 . 308 Mecha...

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... G.A. 88, 91 12 0 Varshavskii, V.Ya. 11 5 12 0 Vasiliev, V.V. 20 28 41 53 64 12 0 15 7, 16 9, 17 4, 18 0 -18 1, 18 3, 215 , 217 222-223 254, 2 61 269 285, 294 300 344 363 379-380, 3 91, 392 ... C.C. 15 6 222 Chen, H J. 239 269 Cherevatsky, A.S. 19 6 222 Chiao, T.T. 77 11 9 18 1 222 Chou, T.W. 15 27 338 363 Crasto, AS. 11 2 -1 13 11 9 Curtis...

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... 0.8 Jute 10 –50 580 22 1. 5 Cotton 15 –40 540 28 1. 5 Wool 75 17 0 5.9 1. 32 Coir 10 –20 250 5.5 1. 5 Bagasse 25 18 0 9 1. 25 Rice 5 15 10 0 6 1. 24 Natural silk 15 400 13 1. 35 Spider silk 4 17 50 12 .7 – Linen – ... f(σ,t,T) (1. 9) 20 Advanced mechanics of composite materials 0 40 80 12 0 16 0 200 2 1 3 4 T,°C T,°C (a) 0 0.2 0.4 0.6 0.8 1 0 0.2 0.4 0.6 0.8 1 0...

Ngày tải lên: 13/08/2014, 08:20

... equations 1 E x = 1 +ν 21 E 1 cos 4 φ + 1 +ν 12 E 2 sin 4 φ − ν 21 E 1 + 1 G 12 sin 2 φ cos 2 φ ν yx E x = ν 21 E 1 −  1 +ν 21 E 1 + 1 +ν 12 E 2 − 1 G 12  sin 2 φ cos 2 φ 1 +ν 21 E 1 cos 2 φ − 1 +ν 12 E 2 sin 2 φ ... A 1 l 2 x1 l 2 y1 +A 2 l 2 x2 l 2 y2 +A 3 l 2 x3 l 2 y3 +A 1 µ 12  l 2 x1 l 2 y2 +l 2 x2 l 2 y1  +A 1 µ 13  l 2 x1...

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... 87, 92, 10 2, 10 5, 10 9, 11 1, 11 4, 13 6, 14 3, 14 5 14 6, 15 7, 240, 247, 292–293, 3 01, 428, 450 polyacrylonitrile (PAN) 12 polyethelene fibers 13 polymeric composites 21 polymeric matrices 18 thermoplastic ... 88 13 1 202 253 Chou, T.W. 16 30 407 434 Crasto, A.S. 12 1 12 2 13 1 Curtis, A.R. 12 1 13 2 Deo, R.B. 472 480 Doxsee, L. 410 435 Dudchenko, A.A. 2 01 254 Egor...

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... Mechanics and analysis of composite materials Goodey, W.J. (19 46). Stress Drymion Problems. Aircraft Eng. June, 19 .5 -19 8; July, 227-234; August, Karpinos, D.M. (19 85). Composite Materials. ... This condition yields the following cubic equation for a ~3 -1, a2-40 -13 =0 , (2 .12 ) 40 Mechanics and analysis of composite materials 2.7. Compatibility eq...

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... a composite pressure vessel. 11 2 Mechanics and analysis of composite materials 01 = 7C2Df + Gm (1 +a) (1 +cos:) cd( 1 + a)a4 2( 1 + (n2Gm /12 @m)) 2Emc ( 1 -cos- y:) , ?r2 (1 ... and analysis of composite materials o,,MPa 2000 16 00 12 00 aoo 4w 0 0 0.5 1 1. 5 (a ) 0 2 ; ~,2. MPa 200 [ 50 p-;2 E2+,' 0 12 % 0 1 2...

Ngày tải lên: 13/08/2014, 17:20