Author: Alfred GessowPublisher:
ISBN:
Category :
Languages : en
Pages : 45
Book Description
A Survey of Computation Aerodynamics in the United States
Author: Alfred GessowA Survey of Computational Aerodynamics in the United States
Author: Alfred GessowA Survey of Computational Aerodynamics in the United States
Author: Alfred GessowPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 60
Book Description
An Introduction to Theoretical and Computational Aerodynamics
Author: Jack MoranPublisher: Courier Corporation
ISBN: 0486317536
Category : Technology & Engineering
Languages : en
Pages : 484
Book Description
Concise text discusses properties of wings and airfoils in incompressible and primarily inviscid flow, viscid flows, panel methods, finite difference methods, and computation of transonic flows past thin airfoils. 1984 edition.
Applied Computational Aerodynamics
Author: Russell M. CummingsPublisher: Cambridge University Press
ISBN: 1107053749
Category : Mathematics
Languages : en
Pages : 893
Book Description
This book covers the application of computational fluid dynamics from low-speed to high-speed flows, especially for use in aerospace applications.
Computational Aerodynamics and Fluid Dynamics
Author: Jean-Jacques ChattotPublisher: Springer Science & Business Media
ISBN: 9783540434948
Category : Mathematics
Languages : en
Pages : 210
Book Description
The book gives the reader the basis for understanding the way numerical schemes achieve accurate and stable simulations of physical phenomena. It is based on the finite-difference method and simple problems that allow also the analytic solutions to be worked out. ODEs as well as hyperbolic, parabolic and elliptic types are treated. The book builds on simple model equations and, pedagogically, on a host of problems given together with their solutions.
Computational Aerodynamics
Author: Antony JamesonPublisher: Cambridge University Press
ISBN: 1108837883
Category : Science
Languages : en
Pages : 627
Book Description
Learn the design and analysis of numerical algorithms for aerodynamics. Ideal for graduates, researchers, and professionals in the field.
Theory of Lift
Author: G. D. McBainPublisher: John Wiley & Sons
ISBN: 1118346289
Category : Technology & Engineering
Languages : en
Pages : 357
Book Description
Starting from a basic knowledge of mathematics and mechanics gained in standard foundation classes, Theory of Lift: Introductory Computational Aerodynamics in MATLAB/Octave takes the reader conceptually through from the fundamental mechanics of lift to the stage of actually being able to make practical calculations and predictions of the coefficient of lift for realistic wing profile and planform geometries. The classical framework and methods of aerodynamics are covered in detail and the reader is shown how they may be used to develop simple yet powerful MATLAB or Octave programs that accurately predict and visualise the dynamics of real wing shapes, using lumped vortex, panel, and vortex lattice methods. This book contains all the mathematical development and formulae required in standard incompressible aerodynamics as well as dozens of small but complete working programs which can be put to use immediately using either the popular MATLAB or free Octave computional modelling packages. Key features: Synthesizes the classical foundations of aerodynamics with hands-on computation, emphasizing interactivity and visualization. Includes complete source code for all programs, all listings having been tested for compatibility with both MATLAB and Octave. Companion website (www.wiley.com/go/mcbain) hosting codes and solutions. Theory of Lift: Introductory Computational Aerodynamics in MATLAB/Octave is an introductory text for graduate and senior undergraduate students on aeronautical and aerospace engineering courses and also forms a valuable reference for engineers and designers.
An Engineering Approach to the Calculation of Aerodynamic Flows
Author: Tuncer CebeciPublisher: Springer
ISBN: 9783642085437
Category : Science
Languages : en
Pages : 396
Book Description
This book describes an engineering approach based on interactive boundary-layer and stability-transition theories, both developed by the author, for calculating aerodynamic flows. This is the first time these powerful computational techniques have been published in book form.
Author: