Computational Fluid Dynamics
The Beginner's guide to Computational Fluid Dynamics From aerospace design to applications in civil, mechanical, and chemical engineering, computational fluid dynamics (CFD) is as essential as it is complex. The most accessible introduction of its kind, Computational Fluid Dynamics: The Basics With Applications, by experienced aerospace engineer John D. Anderson, Jr., gives you a thorough grounding in: the governing equations of fluid dynamics--their derivation, physical meaning, and most relevant forms; numerical discretization of the governing equations--including grids with appropriate transformations and popular techniques for solving flow problems; common CFD computer graphic techiniques; applications of CFD to 4 classic fluid dynamics problems--quasi-one-dimensional nozzle flows, two-dimensional supersonic flow, incompressible couette flow, and supersonic flow over a flat plate; state-of-the-art algorithms and applications in CFD--from the Beam and Warming Method to Second-Order Upwind Schemes and beyond.
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airfoil algorithm application approach artificial viscosity behavior boundary conditions calculation central difference Chap chapter computational fluid dynamics computational plane conservation form continuity equation contour control volume Couette flow denoted density dependent variables described in Sec difference equation direction discussed in Sec domain downstream dx dy elliptic energy equation Euler equations exact analytical example expansion wave explicit finite finite-difference flow field flow problem flow-field variables fluid dynamics flux given by Eq governing equations governing flow equations grid points Hence hyperbolic implicit incompressible initial conditions inviscid flow isentropic iteration Mach number marching mass flow mesh momentum Navier-Stokes equations nonconservation form nondimensional Note nozzle flow numerical results numerical solution parabolic partial differential equations physical plane primitive variables shock wave shown in Fig sketched in Fig solve space specific steady-state subsonic flow surface temperature transformation two-dimensional unsteady values vector velocity profile viscous flow wall