Aeroelasticity is an essential discipline for the design of airplanes, unmanned systems, and innovative configurations.This book introduces the subject of unsteady aerodynamics and dynamic aeroelasticity by presenting industry-standard techniques, such as the Doublet Lattice Method for nonplanar wing systems. "Introduction to Unsteady Aerodynamics and Dynamic Aeroelasticity'' is a useful reference for aerospace engineers and users of NASTRAN and ZAERO but is also an excellent complementary textbook for senior undergraduate and graduate students.  The theoretical material includes:-        Fundamental equations of aerodynamics.-        Concepts of Velocity and Acceleration Potentials.-        Theory of small perturbations.-        Virtual displacements and work, Hamilton's Principle, and Lagrange's Equations.-        Aeroelastic equations expressed in the time, Laplace, and Fourier domains.-       Concept of Generalized Aerodynamic Force Matrix.-       Complete derivation of the nonplanar kernel for unsteady aerodynamic analyses.-       Detailed derivation of the Doublet Lattice Method.-        Linear Time-Invariant systems and stability analysis.-        Rational function approximation for the generalized aerodynamic force matrix.-        Fluid-structure boundary conditions and splining.-        Root locus technique.-        Techniques to find the flutter point:k,k-E,p-k, non-iterativep-k,g, second-orderg,GAAM,p,p-L,p-p, and CV methods.