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 21
... equilibrium equations for plane structures with loads act- ing solely in the x - y plane is reduced from the six for ... equilibrium equations are sufficient to obtain P , V , and M. Since every free body of a plane structure must be in ...
... equilibrium equations for plane structures with loads act- ing solely in the x - y plane is reduced from the six for ... equilibrium equations are sufficient to obtain P , V , and M. Since every free body of a plane structure must be in ...
Page 23
... equilibrium equations written in the example , only six are independent . Since only six independent equilibrium equations exist , there are sev- eral combinations of six of the nine equations that can be considered as independent . The ...
... equilibrium equations written in the example , only six are independent . Since only six independent equilibrium equations exist , there are sev- eral combinations of six of the nine equations that can be considered as independent . The ...
Page 41
... equilibrium equations , so the structure is now statically indeterminate . The construction of structures may include some sort of internal release of continuity of deformation . Concurrent with the release of deformation continuity at ...
... equilibrium equations , so the structure is now statically indeterminate . The construction of structures may include some sort of internal release of continuity of deformation . Concurrent with the release of deformation continuity at ...
Common terms and phrases
acting action analysis applied applied loads assumed assumptions axial force axis beam behavior bending calculation caused Chapter column components Compute condition constant continued create curvature defined deflection deformations developed direction displacement distribution Draw elastic end moments energy equal equations equilibrium equilibrium equations established Example expression Figure fixed force system frame free body function geometric gives hinge horizontal indeterminate structure influence line integration internal joint length limitations linear load magnitude material mathematical matrix maximum member forces ments method Note obtained occur plane positive presented principle Problem provides reaction relation relative rotation shear shown in Fig simple slope solution solve statically determinate STEP stiffness strain stresses structure symmetric Table tion truss unit load unknown vertical virtual yields zero ΕΙ