Book contents
- Frontmatter
- Contents
- Preface
- Preface to the First Edition
- 1 Introduction and Background
- 2 Fundamentals of Inviscid, Incompressible Flow
- 3 General Solution of the Incompressible, Potential Flow Equations
- 4 Small-Disturbance Flow over Three-Dimensional Wings: Formulation of the Problem
- 5 Small-Disturbance Flow over Two-Dimensional Airfoils
- 6 Exact Solutions with Complex Variables
- 7 Perturbation Methods
- 8 Three-Dimensional Small-Disturbance Solutions
- 9 Numerical (Panel) Methods
- 10 Singularity Elements and Influence Coefficients
- 11 Two-Dimensional Numerical Solutions
- 12 Three-Dimensional Numerical Solutions
- 13 Unsteady Incompressible Potential Flow
- 14 The Laminar Boundary Layer
- 15 Enhancement of the Potential Flow Model
- A Airfoil Integrals
- B Singularity Distribution Integrals
- C Principal Value of the Lifting Surface Integral IL
- D Sample Computer Programs
- Index
11 - Two-Dimensional Numerical Solutions
Published online by Cambridge University Press: 05 June 2012
- Frontmatter
- Contents
- Preface
- Preface to the First Edition
- 1 Introduction and Background
- 2 Fundamentals of Inviscid, Incompressible Flow
- 3 General Solution of the Incompressible, Potential Flow Equations
- 4 Small-Disturbance Flow over Three-Dimensional Wings: Formulation of the Problem
- 5 Small-Disturbance Flow over Two-Dimensional Airfoils
- 6 Exact Solutions with Complex Variables
- 7 Perturbation Methods
- 8 Three-Dimensional Small-Disturbance Solutions
- 9 Numerical (Panel) Methods
- 10 Singularity Elements and Influence Coefficients
- 11 Two-Dimensional Numerical Solutions
- 12 Three-Dimensional Numerical Solutions
- 13 Unsteady Incompressible Potential Flow
- 14 The Laminar Boundary Layer
- 15 Enhancement of the Potential Flow Model
- A Airfoil Integrals
- B Singularity Distribution Integrals
- C Principal Value of the Lifting Surface Integral IL
- D Sample Computer Programs
- Index
Summary
The principles of singular element based numerical solutions were introduced in Chapter 9 and the first examples are provided in this chapter. The following two-dimensional examples will have all the elements of more refined three-dimensional methods, but because of the simple two-dimensional geometry, the programming effort is substantially less. Consequently, such methods can be developed in a short time for investigating improvements in larger codes and are also suitable for homework assignments and class demonstrations.
Based on the level of approximation of the singularity distribution, surface geometry, and type of boundary conditions, numerous computational methods can be constructed, some of which are presented in Table 11.1. We will not attempt to demonstrate all the possible combinations but will try to cover some of the most frequently used methods (denoted by the word “example” in Table 11.1), including discrete singular elements and constant-strength, linear, and quadratic elements (as an example for higher order singularity distributions). The different approaches in specifying the zero normal velocity boundary condition will be exercised and mainly the outer Neumann normal velocity and the internal Dirichlet boundary conditions will be used (and there are additional options, e.g., an internal Neumann condition). In terms of the surface geometry, for simplicity, only the flat panel element will be used here and in areas of high surface curvature the solution can be improved by using more panels.
In this chapter and in the following ones the primary concern is the simplicity of the explanation and the ease of constructing the numerical technique, while numerical efficiency considerations are secondary.
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- Low-Speed Aerodynamics , pp. 262 - 330Publisher: Cambridge University PressPrint publication year: 2001