david roylance mechanics of materials Part 8 doc

... -0.1228D-15 0.2228D-19 0.7218E-10 0.1 084 E- 18 -0.6022E-16 0.3058D-09 -0.4265D-11 -0.1967D-15 0.6214E-22 -0.7218E-10 -0.1228E-15 -0.4265D-11 0.3058D-09 -0.2 580 D-14 -0.6022E-16 -0.1228E-15 0.2228E-19 -0.1967D-15 ... matrix: 0.2548E-10 -0.3554E-12 -0.1639E-16 0.7218D-10 0.7125D-19 -0.6022D-16 -0.3554E-12 0.2548E-10 -0.2150E-15 0.3253D- 18 -0.7218D-10 -0.1228D-15 -0.1639E-16 -0.2150E-15 0.2...

Ngày tải lên: 11/08/2014, 02:21

... 0 .81 59 0 .81 86 0 .82 12 0 .82 38 0 .82 64 0 .82 89 0 .83 15 0 .83 40 0 .83 65 0 .83 89 1.0 0 .84 13 0 .84 38 0 .84 61 0 .84 85 0 .85 08 0 .85 31 0 .85 54 0 .85 77 0 .85 99 0 .86 21 1.1 0 .86 43 0 .86 65 0 .86 86 0 .87 08 0 .87 29 0 .87 49 0 .87 70 ... 0. 981 7 2.1 0. 982 1 0. 982 6 0. 983 0 0. 983 4 0. 983 8 0. 984 2 0. 984 6 0. 985 0 0. 985 4 0. 985 7 2.2 0. 986 1 0. 986 4 0. 986 8 0....

Ngày tải lên: 11/08/2014, 02:21

... mathematician Simeon Denis Poisson, (1 781 – 184 0). 6 SHEAR AND TORSION David Roylance Department of Materials Science and Engineering Massachusetts Institute of Technology Cambridge, MA 02139 June ... Advanced Strength of Materials, McGraw-Hill, New York, 1952 12 The Kinematic Equations David Roylance Department of Materials Science and Engineering Massachusetts Institu...

Ngày tải lên: 11/08/2014, 02:21

... + ∂u ∂y dy 13 Transformation of Stresses and Strains David Roylance Department of Materials Science and Engineering Massachusetts Institute of Technology Cambridge, MA 02139 May 14, 2001 Introduction One of the most ... RAR −1       x  y γ xy      3 The Equilibrium Equations David Roylance Department of Materials Science and Engineering Massachusetts Institut...

Ngày tải lên: 11/08/2014, 02:21

... are δ ij  kk = δ ij σ kk 3K =   0.0 289 0 0 00.0 289 0 000.0 289   e ij = Σ ij 2G =   00.03 78 0.0441 0.03 78 0.0 189 0.0567 0.0441 0.0567 −0.0 189   The total strain is then  ij = 1 3  kk δ ij + e ij =   0.00960 0.03 78 0.0441 0.03 78 ... couple. The first five of these functions are sketched in Fig. 11. 8 STRESSES IN BEAMS David Roylance Department of Materials...

Ngày tải lên: 11/08/2014, 02:21

... = 0, c1 = -87 .82 , Rb = 93. 78, Ra = 28. 11, Rc = 28. 11} > # assign the known values for plotting purposes: > c1:= -87 .82 ;c2:=0;Ra:= 28. 11;Rb:=93. 78; Rc:= 28. 11; > # the equation of the deflection ... Stress and Strain, McGraw-Hill, New York, 1 989 . 9 Beam Displacements David Roylance Department of Materials Science and Engineering Massachusetts Institute of Techn...

Ngày tải lên: 11/08/2014, 02:21

... DOF 1 DOF 2 DOF 3 DOF 4 DOF 5 DOF 6 1 000000 2 0.013333 -0.03219 0000 3 0.02 -0. 084 379 0000 4 000000 5 -0.0066667 -0.0 388 56 0000 Element Stresses 1: 4000 2: 2000 3: - 282 8.4 4: 2000 5: - 282 8.4 6: ... e 2α 0 )sinhζ −e 2α 0 cosh ζ] 8 Finite Element Analysis David Roylance Department of Materials Science and Engineering Massachusetts Institute of Technology Cambridge, MA 0...

Ngày tải lên: 11/08/2014, 02:21

... material=steel 2 nodes=[67, 58, 55] 6 nodes=[50,41,40] . . . 7 nodes=[ 68, 67,69] load=load_case_1 8 nodes=[ 68, 58, 67] 9 nodes=[57, 58, 68] load=load_case_1 10 nodes=[57,51, 58] 11 nodes=[52,51,57] load=load_case_1 12 ... constraint=slide_x 2 x=1.19644 y=-0 z=0 3 x=0. 984 562 y=0.167939 z=0 constraint=free 4 x=0.940634 y=0.33 584 1 z=0 5 x=1.0 788 8 y=0.23 583 3 z=0 . . . 72 x=3.99602 y=...

Ngày tải lên: 11/08/2014, 02:21