Technical Abstract Bulletin
Author : Defense Documentation Center (U.S.)
Publisher :
Page : 784 pages
File Size : 36,62 MB
Release : 1967
Category : Science
ISBN :
Author : Defense Documentation Center (U.S.)
Publisher :
Page : 784 pages
File Size : 36,62 MB
Release : 1967
Category : Science
ISBN :
Author :
Publisher :
Page : 702 pages
File Size : 34,56 MB
Release : 1995
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 1352 pages
File Size : 45,58 MB
Release : 1967
Category : Government publications
ISBN :
Author : Charles R. Strom
Publisher :
Page : 136 pages
File Size : 34,33 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 : J. B. Moreno
Publisher :
Page : 136 pages
File Size : 17,23 MB
Release : 1967
Category : Aerodynamics, Supersonic
ISBN :
Two flow-field computer codes are described. The codes were developed to compute the flow about blunt axisymmetric or two-dimensional bodies moving with supersonic speeds at zero angle of attack. Boundary-layer effects and a variety of thermochemical options are included. A pair of auxiliary codes for machine-plotting the flow-field results is also described.
Author : H. J. Fivel
Publisher :
Page : 130 pages
File Size : 13,71 MB
Release : 1975
Category : Aerodynamics, Hypersonic
ISBN :
Author :
Publisher :
Page : 670 pages
File Size : 44,50 MB
Release : 1968
Category : Science
ISBN :
Author :
Publisher :
Page : 956 pages
File Size : 35,38 MB
Release : 1970-05
Category : Science
ISBN :
Author :
Publisher :
Page : 954 pages
File Size : 50,42 MB
Release : 1973
Category : Government publications
ISBN :
Author :
Publisher :
Page : 744 pages
File Size : 41,85 MB
Release : 1970
Category : Science
ISBN :