The representation of the stress and strain tensors and the formulation of the boundary-value problem of linear elasticity in cylindrical coordinates is considered. The Cauchy equations of equilibrium, expressed in terms of stresses, the strain–displacement relations, the compatibility equations, the generalized Hooke's law, and the Navier equations of equilibrium, expressed in terms of displacements, are all cast in cylindrical coordinates. The axisymmetric boundary-value problem of a pressurized hollow cylinder with either open or closed ends is formulated and solved. The results are used to obtain the elastic fields for a pressurized circular hole in an infinite medium, and to solve a cylindrical shrink-fit problem. A pressurized hollow sphere and a spherical shrink-fit problem are also considered to illustrate the solution procedure in the case of problems with spherical symmetry.

Partial differential equations whose solution specifies the elastic response of a loaded body are summarized. If all boundary conditions are given in terms of tractions, the boundary-value problem can be specified entirely in terms of stresses. The governing differential equations are then the Cauchy equations of equilibrium and the Beltrami–Michell compatibility equations. If some of the boundary conditions are given in terms of the displacements, the boundary-value problem is formulated in terms of the displacement components through the Navier equations of equilibrium. The boundary conditions can be expressed in terms of displacements, or in terms of displacement gradients. Due to the linearity of all equations and boundary conditions, the principle of superposition applies in linear elasticity. The semi-inverse method of solution and the Saint-Venant principle are introduced and discussed. The solution procedure is illustrated in the analysis of the stretching of a prismatic bar by its own weight, thermal expansion of a compressed prismatic bar, pure bending of a prismatic bar, and torsion of a prismatic rod with a circular cross section.