Low-speed aerodynamics is important in the design and operation of aircraft flying at low Mach number, and ground and marine vehicles. This text offers a modern treatment of both the theory of inviscid, incompressible, and irrotational aerodynamics, and the computational techniques now available to solve complex problems. A unique feature is that the computational approach—from a single vortex element to a three-dimensional panel formulation—is interwoven throughout. This second edition...
Modern treatment of low-speed aerodynamics, covering both theory and computational techniques.
PrefacePreface to the First Edition1Introduction and Background12Fundamentals of Inviscid, Incompressible Flow213General Solution of the Incompressible, Potential Flow Equations444Small-Disturbance Flow over Three-Dimensional Wings: Formulation of the Problem755Small-Disturbance Flow over Two-Dimensional Airfoils946Exact Solutions with Complex Variables1227Perturbation Methods1518Three-Dimensional Small-Disturbance Solutions1679Numerical (Panel) Methods20610Singularity Elements and Influence Coefficients23011Two-Dimensional Numerical Solutions26212Three-Dimensional Numerical Solutions33113Unsteady Incompressible Potential Flow36914The Laminar Boundary Layer44815Enhancement of the Potential Flow Model483AAirfoil Integrals537BSingularity Distribution Integrals540CPrincipal Value of the Lifting Surface Integral I[subscript L]545DSample Computer Programs546Index611