Three-dimensional Flow of Ideal Gas Past Smooth Bodies
Author : Konstantin Ivanovich Babenko
Publisher :
Page : 532 pages
File Size : 25,67 MB
Release : 1966
Category : Aerodynamics
ISBN :
Author : Konstantin Ivanovich Babenko
Publisher :
Page : 532 pages
File Size : 25,67 MB
Release : 1966
Category : Aerodynamics
ISBN :
Author : Konstantin Ivanovich Babenko
Publisher :
Page : 520 pages
File Size : 25,54 MB
Release : 1968
Category : Aerodynamics
ISBN :
Author : K. I. Babenko
Publisher :
Page : pages
File Size : 36,1 MB
Release : 1968
Category : Gas
ISBN :
Author : K. I. Babenko
Publisher :
Page : pages
File Size : 17,89 MB
Release : 1965
Category : Aerodynamics
ISBN :
Author :
Publisher :
Page : 517 pages
File Size : 29,17 MB
Release : 1966
Category : Aerodynamics
ISBN :
Author : Charles R. Strom
Publisher :
Page : 136 pages
File Size : 24,55 MB
Release : 1967
Category : Aerodynamics
ISBN :
The method of characteristics is formulated for the computation of the supersonic flow of an inviscid, reacting gas over a smooth three-dimensional body. Various methods of constructing networks of bicharacteristic lines are examined from the point of view of numerical stability and accuracy. A new method of forming the network, which consists of projecting forward along streamlines from data points on specified data planes, is found to be most easily adopted to the particular requirements of nonequilibrium chemistry. The general method was coded for the IBM 7090 computer and the program demonstrated for the case of an ideal gas. Calculations were made for the case of an ideal gas. Calculations were made for the flow about a spherical-tip 15 degree half-angle cone at 10 degree angle of attack and a generalized elliptical body at zero incidence. Since the program yields the pressure distribution along specified streamlines, it is straightforward, in principle, to link it to a finite-rate chemistry stream tube program to treat three-dimensional, nonequilibrium flows. (Author).
Author :
Publisher :
Page : 912 pages
File Size : 28,29 MB
Release : 1976
Category : Science
ISBN :
Author : D. Küchemann
Publisher : Elsevier
Page : 481 pages
File Size : 12,72 MB
Release : 2014-12-02
Category : Technology & Engineering
ISBN : 1483224880
Progress in Aeronautical Sciences, Volume 9 presents the vibrational characteristics of certain aircraft. This book supplements the comprehensive account of matrix methods of structural analysis. Organized into five chapters, this volume begins with an overview of the different schemes of the numerical method of characteristics for calculating three-dimensional steady supersonic gas flow about bodies moving at incidence. This text then examines the flow of a perfect gas and provides the generalization for the case of equilibrium and non-equilibrium flow of real gas. Other chapters consider the various aspects of the aerodynamic design of aircraft and discuss the application of modern computer methods to fluid mechanics. This book discusses as well the prospects for further development of the existing types and for the establishment of the as yet hypothetical types of aircraft. The final chapter shows how the evolution of the aerodynamic shape leads to a complete spectrum of major types of aircraft. This book is a valuable resource for engineers.
Author :
Publisher :
Page : 1390 pages
File Size : 21,77 MB
Release : 1987
Category : Aeronautics
ISBN :
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author :
Publisher :
Page : 758 pages
File Size : 28,7 MB
Release : 1970
Category : Aerodynamics
ISBN :