NASA Technical Memorandum
Author :
Publisher :
Page : 220 pages
File Size : 11,69 MB
Release : 1984
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 220 pages
File Size : 11,69 MB
Release : 1984
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 62 pages
File Size : 26,65 MB
Release : 1992
Category : Science
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 380 pages
File Size : 30,75 MB
Release : 1990
Category : Aeronautics
ISBN :
Author : Russell M. Cummings
Publisher : Cambridge University Press
Page : 893 pages
File Size : 11,80 MB
Release : 2015-04-27
Category : Technology & Engineering
ISBN : 1316240290
This computational aerodynamics textbook is written at the undergraduate level, based on years of teaching focused on developing the engineering skills required to become an intelligent user of aerodynamic codes. This is done by taking advantage of CA codes that are now available and doing projects to learn the basic numerical and aerodynamic concepts required. This book includes a number of unique features to make studying computational aerodynamics more enjoyable. These include: • The computer programs used in the book's projects are all open source and accessible to students and practicing engineers alike on the book's website, www.cambridge.org/aerodynamics. The site includes access to images, movies, programs, and more • The computational aerodynamics concepts are given relevance by CA Concept Boxes integrated into the chapters to provide realistic asides to the concepts • Readers can see fluids in motion with the Flow Visualization Boxes carefully integrated into the text.
Author :
Publisher :
Page : 604 pages
File Size : 15,47 MB
Release : 1974
Category :
ISBN :
Author :
Publisher :
Page : 704 pages
File Size : 45,28 MB
Release : 1995
Category : Aeronautics
ISBN :
Author : Harry W. Carlson
Publisher :
Page : 44 pages
File Size : 14,59 MB
Release : 1979
Category :
ISBN :
Author : Charles E. Mercer
Publisher :
Page : 204 pages
File Size : 17,53 MB
Release : 1979
Category :
ISBN :
Author : Josef Rom
Publisher : Springer Science & Business Media
Page : 408 pages
File Size : 17,62 MB
Release : 2012-12-06
Category : Science
ISBN : 1461228247
The aerodynamics of aircraft at high angles of attack is a subject which is being pursued diligently, because the modern agile fighter aircraft and many of the current generation of missiles must perform well at very high incidence, near and beyond stall. However, a comprehensive presentation of the methods and results applicable to the studies of the complex aerodynamics at high angle of attack has not been covered in monographs or textbooks. This book is not the usual textbook in that it goes beyond just presenting the basic theoretical and experimental know-how, since it contains reference material to practical calculation methods and technical and experimental results which can be useful to the practicing aerospace engineers and scientists. It can certainly be used as a text and reference book for graduate courses on subjects related to high angles of attack aerodynamics and for topics related to three-dimensional separation in viscous flow courses. In addition, the book is addressed to the aerodynamicist interested in a comprehensive reference to methods of analysis and computations of high angle of attack flow phenomena and is written for the aerospace scientist and engineer who is familiar with the basic concepts of viscous and inviscid flows and with computational methods used in fluid dynamics.
Author : Richard E. Meyer
Publisher : Academic Press
Page : 356 pages
File Size : 25,12 MB
Release : 2014-05-10
Category : Technology & Engineering
ISBN : 1483264602
Mathematics Research Center Symposium: Transonic, Shock, and Multidimensional Flows: Advances in Scientific Computing covers the lectures presented at a Symposium on Transonic, Shock, and Multidimensional Flows, held in Madison on May 13-15, 1981, under the auspices of the Mathematics Research Center of the University of Wisconsin. The book focuses on the advancements in the scientific computation of high-speed aerodynamic phenomena and related fluid motions. The selection first elaborates on computational fluid dynamics of airfoils and wings; shock-free configurations in two- and three-dimensional transonic flow; and steady-state solution of the Euler equations for transonic flow. Discussions focus on boundary conditions, convergence acceleration, indirect design of airfoils, and trailing edge and the boundary layer. The text then examines the calculation of transonic potential flow past three-dimensional configurations and remarks on the numerical solution of Tricomi-type equations. The manuscript ponders on the design and numerical analysis of vortex methods, shock calculations and the numerical solution of singular perturbation problems, tracking of interfaces for fluid flow, and transonic flows with viscous effects. Topics include numerical algorithm, difference approximation for scalar equations, boundary conditions, transonic flow in a tube, and governing equations. The selection is a dependable reference for researchers interested in transonic, shock, and multidimensional flows.