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. |
From inside the book
Results 1-3 of 3
Page 199
... thickness ratios for compression elements in such cross sections are set in design codes and specifications to ensure the performance of the cross section as assumed in simple bending theory ( References 3 , 6 , 8 , 15 , and 39 ) . The ...
... thickness ratios for compression elements in such cross sections are set in design codes and specifications to ensure the performance of the cross section as assumed in simple bending theory ( References 3 , 6 , 8 , 15 , and 39 ) . The ...
Page 340
... thickness is constant . Numerical integration of Eq . ( 6.14 ) is used in this problem and the results are compared with the exact val- ues of the integral for different t / D ratios . The details of the numerical computations are not ...
... thickness is constant . Numerical integration of Eq . ( 6.14 ) is used in this problem and the results are compared with the exact val- ues of the integral for different t / D ratios . The details of the numerical computations are not ...
Page 341
Edwin C. Rossow. The tapered tube of constant wall thickness is subjected to a uniform applied force per unit length , p . Compute the displacement of the right end . Take E as constant , and compute A. A = = - - π [ D2 ( x ) − ( D ( x ) ...
Edwin C. Rossow. The tapered tube of constant wall thickness is subjected to a uniform applied force per unit length , p . Compute the displacement of the right end . Take E as constant , and compute A. A = = - - π [ D2 ( x ) − ( D ( x ) ...
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