The basic algorithmic elements for solving hyperbolic, elliptic, and parabolic equations presented in the opening chapters are applied to solving the transonic small disturbance equations, the full potential equation, the Euler equations, and the Navier-Stokes equations. Examples apply numerical procedures for solving one-dimensional Euler equations to flow within a supersonic inlet, a converging-diverging nozzle, and a piston tube, and flow past an expansion corner and a compression corner. Two-dimensional Euler equations calculate supersonic flow past a wedge, subsonic and transonic flow past a circular arc airfoil, subsonic flow past an ellipse, and supersonic flow past a cone. Annotation ©2014 Ringgold, Inc., Portland, OR (protoview.com)