The paper gives exact solutions to the stability and vibration problems for nonclosed circular cylindrical shells hinged along the longitudinal edges and reinforced with a regularly arranged discrete longitudinal ribs. These problems are also solved approximately in the cases of regularly and quasiregularly arranged ribs Keywords: nonclosed circular cylindrical shell, discrete longitudinal ribs, stability and vibrations, exact solution, approximate solutionIntroduction. The deformation of nonclosed cylindrical shells with discrete longitudinal ribs came to be studied even in the middle of the last century [1]. Those studies used methods that represent solutions in the form of single trigonometric series. These solutions are inconvenient when there are either few ribs (they lead to ill-conditioned systems of linear algebraic equations) or many ribs (they lead to very large systems of equations). The finite-element method (see, e.g., [8,12,13]) and the finite-difference method (see, e.g., [10]) make the application of single trigonometric series for shells with discrete ribs noncompetitive, unlike analytic methods based on asymptotic methods [2,6,7,9,16,23] or double trigonometric series [2,3,5,6,16]. The latter allow obtaining, in some cases, exact solutions in convenient form to the equations of motion and, as asymptotic methods, simple approximate formulas suitable for analysis of the deformation of shells without labor-intensive calculations.In what follows, we will analyze the stability and vibrations of nonclosed cylindrical shells reinforced with discrete longitudinal edges under longitudinal compression and external (internal) pressure. The exact solution of the equations of motion will be obtained for shells reinforced with a regular system of ribs (all ribs have equal stiffness and mechanical characteristics and are equally spaced, and the distance from the extreme ribs to the longitudinal edges of the shell are equal to the distance between ribs). The critical stresses (natural frequencies, wave numbers) are determined by finding the roots of transcendental equations. For shells reinforced with a "quasiregular" system of ribs (the distance from the extreme edges to longitudinal ribs equals half the distance between ribs) as well as for shells reinforced with a regular system of ribs, we will derive simple approximate formulas based on the Bubnov-Galerkin method and the monomial approximation of the displacement components. The stability of circular closed cylindrical shells reinforced with a quasiregular system of rings was analyzed in [2]. Solutions to some other problems for closed cylindrical shells are presented in [14,15,[17][18][19][20][21][22].1. Equations of Motion. The equations of motion for a thin elastic nonclosed circular cylindrical shell reinforced with discrete longitudinal ribs were derived in [2] assuming that the subcritical state of the shell is momentless. We will generalize them to the stability problems addressed below. These equations can be written as