Analysis and Behavior of StructuresOffering students a presentation of classical structural analysis, this text emphasizes the limitations required in creating mathematical models for analysis, including these used in computer programs. Students are encouraged to use hand methods of analysis to develop a feel for the behaviour of structures. |
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Page 236
... determine the loca- tion of the maximum vertical deflection of the structure shown . Compute the deflection at that point in feet ( EI constant = 1.45 x 106 kip - in2 ) . 2k / ft A TOT B 17 10 ' +3 ' — 10K 10K Hinge 6.2 Use the ...
... determine the loca- tion of the maximum vertical deflection of the structure shown . Compute the deflection at that point in feet ( EI constant = 1.45 x 106 kip - in2 ) . 2k / ft A TOT B 17 10 ' +3 ' — 10K 10K Hinge 6.2 Use the ...
Page 364
... Determine the moment of inertia of the beam as a function of x . ( b ) For the loading shown , obtain an approximate value of the deflection of the left end of the beam . Use Simpson's rule to evaluate any integrals in the com- putation ...
... Determine the moment of inertia of the beam as a function of x . ( b ) For the loading shown , obtain an approximate value of the deflection of the left end of the beam . Use Simpson's rule to evaluate any integrals in the com- putation ...
Page 430
... Determine the deflection of the center of the beams when the load P ( in the negative z direction ) is applied ( E constant ) . Z P 3 गिरीश 100 kN . B 21 C T A M D 3.6 m 1.5 m 3.9 m 1.5 m + 2/2 2/2 21 THITT 2/2 10.27 Draw the final ...
... Determine the deflection of the center of the beams when the load P ( in the negative z direction ) is applied ( E constant ) . Z P 3 गिरीश 100 kN . B 21 C T A M D 3.6 m 1.5 m 3.9 m 1.5 m + 2/2 2/2 21 THITT 2/2 10.27 Draw the final ...
Common terms and phrases
action analysis antisymmetric applied loads assumption axial loads calculation centroidal column complementary virtual Compute concentrated load conjugate beam constant cross section curvature diagram defined deformation system direct integration displacements and rotations distributed load Draw the final end moments equations of equilibrium equilibrium equations Example Figure final moment diagram forces and moments free body hinge horizontal indeterminate structure influence line integration joint kips kN/m left end linear linear elastic loading diagram magnitude mathematical model maximum member A-B member forces ment moment distribution moment of inertia Neglect axial deformations nonlinear materials nonprismatic numerical integration panel points positive reaction components shown in Fig sign convention simply supported beam slope spreadsheet statically determinate structures STEP strain energy stress stress-strain relation struc superposition tion truss U₁ uniform load unit load vertical deflection vertical displacement virtual force system virtual work principle zero ΕΙ