An Introduction to Theoretical and Computational AerodynamicsThis advanced aerodynamics text shows students how to apply a wide range of computational methods to prepare them to practice professionally. The book presents in an accessible manner both classical and modern developments in computational aerodynamics. Includes listings of FORTRAN computer programs that implement methods developed in the text. |
Contents
WINGS | 1 |
REVIEW OF BASIC FLUID DYNAMICS | 11 |
INCOMPRESSIBLE IRROTATIONAL FLOW ABOUT | 32 |
Copyright | |
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Common terms and phrases
aerodynamic airfoil angle of attack axis Bernoulli's equation body surface boundary conditions boundary layer C₁ calculated camber Chapter chord compute constant coordinates derivatives differential equation direction doublet distribution ellipse evaluate flow past fluid particle force formula incompressible induced drag INPUT integral equation irrotational ith panel Kutta condition laminar Laplace equation leading edge lift coefficient linear mesh molecules momentum NACA Navier-Stokes equations no-slip condition nodes normal onset flow panel method plane pressure distribution pressure gradient PRINT problem RETURN END Reynolds number satisfy shear stress shown in Fig solution solve source distribution source strength stagnation point stream function streamline SUBROUTINE tangential thin-airfoil theory trailing edge two-dimensional upstream V₁ vector velocity components velocity field velocity potential viscous vortex strength vortices wing x₁ zero θο ди дф