This work addresses the aeroelasticity of airfoils with permeable trailing sections which is a topic that has not been studied in the literature before. There has been an increasing interest in the past few years regarding the analysis of permeable airfoils from the aerodynamics and aeroacoustics points of view. So, this work adds a new aspect to the analysis by considering the airfoil elasticity and flexibility effect. Two types of airfoils are considered: membrane airfoils and flexible-chord airfoils. Both static and dynamic aeroelastic studies of permeable airfoils are presented through a parametric analysis to investigate the effects of the permeable section length, permeability factor, boundary conditions represented by the membrane fixed or elastic supports and the elastic center position of flexible-chord airfoils, and the elastic properties of the airfoils like the bending rigidity of flexible-chord airfoils and the tension coefficient of membrane airfoils. The aeroelastic model of permeable airfoils is derived using the Hamilton's variational principle and the finite element method. The finite element system of equations is presented in a time domain nonlinear form to account for the nonlinear stiffening of membrane airfoils. The seepage flow through the permeable section is modeled using Darcy's law. The effects of permeability on the static aerodynamic coefficients, the dynamic response under a sinusoidal gust, and the aeroelastic instabilities (divergence and flutter) are investigated. The study aims at the aeroelastic performance of permeable airfoils subjected to incompressible airflows at small angles of attack and moderate to high Reynolds numbers, so the potential flow theory is adopted for the aerodynamic modeling. The analysis shows that permeability can have a significant effect on the aeroelastic responses of airfoils. The trailing permeable section changes the pressure distribution which changes the lift curve slope and the aerodynamic center position which in turn affects the aeroelastic instabilities and responses. This permeability effect strongly depends on the airfoil's stiffness represented by the bending rigidity of the flexible-chord airfoils and the tension in the membrane airfoils.