Theory of Matrix Structural Analysis
Courier Corporation, 1. 1. 1985 - Počet stran: 468
This pioneering aerospace engineering text belongs on the shelf of every aerospace and structural engineering graduate student and professional engineer. Originally published in 1968, the treatment remains a valuable guide, tracing each procedure in a clear, step-by-step fashion and employing minimal mathematical rigor in its examples.
The text begins with an overview of matrix methods and their application to the structural design of modern aircraft and aerospace vehicles. Subsequent chapters cover the basic equations of elasticity, energy theorems, structural idealization, Castigliano's theorem, derivation of stiffness matrices from flexibility, and constant-shear-flow panels. Additional subjects include a comparison of force and displacement methods, analysis of substructures, structural synthesis, and nonlinear structural analysis. Abundant end-of-chapter supplements provide materials for classroom use.
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Areas of Structural Analysis
Energy Theorems Based on the Principle of Virtual work
INERTIA PROPERTIES of STRUCTURAL ELEMENTS
Další vydání - Zobrazit všechny
analysis applied assumed attached beam element becomes bending body boundary calculated coefficients column compatibility complementary complete concentrated consider constant continuous coordinate system corresponding datum deflection deformation degrees of freedom derived determined direction displacement method displacements distribution elastic element forces elimination energy equal equations equivalent example expressed external forces flexibility follows force method functions given Hence idealization integration introduced joint leads linearly loading mass method moments node noted obtained panel pin-jointed bar plate plate element points presented principle problems properties reactions rectangular plate redundant reference relationship relative represents respectively rigid-body rotations satisfy selected shear shown in Fig ſº solution specified statically stiffness matrix strain strain energy stress structural elements subjected Substituting substructure temperature theorem thermal unit values varying zero