Book Description
Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.
Author : G. N. Ward
Publisher : Cambridge University Press
Page : 261 pages
File Size : 27,20 MB
Release : 2016-02-25
Category : Mathematics
ISBN : 1316601897
Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.
Author :
Publisher : CUP Archive
Page : 268 pages
File Size : 19,50 MB
Release :
Category :
ISBN :
Author : John R. Spreiter
Publisher :
Page : 60 pages
File Size : 44,76 MB
Release : 1959
Category : Aerodynamics
ISBN :
Summary: Approximate solutions of the nonlinear equations of the small disturbance theory of transonic flow are found for the pressure distribution on pointed slender bodies of revolution for flows with free-stream Mach number 1, and for flows that are either purely subsonic or purely supersonic. These results are obtained by application of a method based on local linearization that was introduced recently in the analysis of similar problems in low-dimensional flows. The theory is developed for bodies of arbitrary shapes, and specific results are given for cone-cylinders and for parabolic-arc bodies at zero angle of attack. All results are compared either with existing theoretical results or with experimental data.
Author : Shih-I Pai
Publisher : CRC Press
Page : 724 pages
File Size : 47,5 MB
Release : 2020-11-26
Category : Mathematics
ISBN : 1000152901
This book gives an introduction to the theoretical and computational fluid dynamics of a compressible fluid. It focuses on the basic assumptions and the formulation of the theory of compressible flow as well as on the methods of solving problems.
Author : Pai
Publisher : CRC Press
Page : 724 pages
File Size : 33,24 MB
Release : 1997-03-01
Category : Mathematics
ISBN : 9780442303105
Emphasis of this text is on the basic assumptions and the formulation of the theory of compressible flow as well as on the methods of solving problems. Published by Science Press, Beijing, distributed by VNR in the US. Annotation copyrighted by Book News, Inc., Portland, OR
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 454 pages
File Size : 14,21 MB
Release : 1958
Category : Aeronautics
ISBN :
Author : A. Cemal Eringen
Publisher : Academic Press
Page : 676 pages
File Size : 38,26 MB
Release : 2013-10-22
Category : Science
ISBN : 1483276716
Elastodynamics, Volume II: Linear Theory is a continuation of Volume I and discusses the dynamical theory of linear isotropic elasticity. The volume deals with the fundamental theorems regarding elastodynamics and the different mathematical methods of solution and their employment in one, two, and three dimensions. The text outlines the fundamentals of linear elastodynamics and explains basic equations, displacement formulation, stress formulation, and the uniqueness theorem of elastodynamics. The book also investigates elastodynamic problems involving one-space dimension in governing boundaries, equations, and initial conditions. The book then compares two-dimensional problems as being subject to more precise mathematical analysis compared to three-dimensional situations by using scalar wave equations. The text then analyzes elastodynamic problems in three space dimensions when the solution depends on the condition of separability of the vector wave equation and the satisfaction of the boundary conditions. The diffraction of elastic waves is also described using two approaches: the integral equation method or the Eigen function technique. The book can prove valuable to researchers and practitioners whose work involves advanced statistics, general physics, and thermodynamics.
Author :
Publisher :
Page : 64 pages
File Size : 41,46 MB
Release : 1959
Category : Aerodynamics
ISBN :
Author :
Publisher :
Page : 1130 pages
File Size : 46,87 MB
Release : 1955
Category : Aeronautics
ISBN :
Author : Joseph Katz
Publisher : Cambridge University Press
Page : 636 pages
File Size : 14,68 MB
Release : 2001-02-05
Category : Mathematics
ISBN : 9780521665520
Low-speed aerodynamics is important in the design and operation of aircraft flying at low Mach number, and ground and marine vehicles. This 2001 book offers a modern treatment of the subject, both the theory of inviscid, incompressible, and irrotational aerodynamics and the computational techniques now available to solve complex problems. A unique feature of the text is that the computational approach (from a single vortex element to a three-dimensional panel formulation) is interwoven throughout. Thus, the reader can learn about classical methods of the past, while also learning how to use numerical methods to solve real-world aerodynamic problems. This second edition has a new chapter on the laminar boundary layer (emphasis on the viscous-inviscid coupling), the latest versions of computational techniques, and additional coverage of interaction problems. It includes a systematic treatment of two-dimensional panel methods and a detailed presentation of computational techniques for three-dimensional and unsteady flows. With extensive illustrations and examples, this book will be useful for senior and beginning graduate-level courses, as well as a helpful reference tool for practising engineers.