Book Description
Unified, self-contained view of nonequilibrium effects, body geometries, and similitudes available in hypersonic flow and thin shock layer; appropriate for graduate-level courses in hypersonic flow theory. 1966 edition.
Author : Wallace D. Hayes
Publisher : Courier Corporation
Page : 628 pages
File Size : 50,98 MB
Release : 2012-07-13
Category : Science
ISBN : 0486160483
Unified, self-contained view of nonequilibrium effects, body geometries, and similitudes available in hypersonic flow and thin shock layer; appropriate for graduate-level courses in hypersonic flow theory. 1966 edition.
Author : John Timothy Suttles
Publisher :
Page : 68 pages
File Size : 17,47 MB
Release : 1969
Category : Heat
ISBN :
Author : E. B. Klunker
Publisher :
Page : 92 pages
File Size : 39,28 MB
Release : 1971
Category : Aerodynamics, Supersonic
ISBN :
A computational technique, called the method of lines, is developed for computing the flow field about conical configurations at incidence in a supersonic flow. The method, which makes use of the self-similarity property, is developed for the nonlinear flow equations. The method has proved to be an efficient and versatile procedure for constructing the numerical solutions to conical flow problems. It has been successful in computing the flow about circular and elliptic cones at conditions where small regions of supersonic cross flow develop and for the conical delta wings where the region of supersonic cross flow is extensive. The calculations made for circular and elliptic cones as well as for the compression side of various conical delta wings are in good agreement with experiment except in regions where viscous effects become important.
Author : John David Anderson (Jr.)
Publisher :
Page : 78 pages
File Size : 17,61 MB
Release : 1968
Category : Aerodynamics, Hypersonic
ISBN :
New results are presented for inviscid, supersonic and hypersonic blunt-body flow fields obtained with a numerical time-dependent method patterned after that of Moretti and Abbett. In addition, important comments are made with regard to the physical and numerical nature of the method. Specifically, numerical results are presented for two-dimensional and axisymmetric parabolic and cubic blunt bodies as well as blunted wedges and cones; these results are presented for zero degrees angle of attack and for a calorically perfect gas with gamma = 1.4. The numerical results are compared with other existing theoretical and experimental data. Also, the effects of initial conditions and boundary conditions are systematically examined with regard to the convergence of the time-dependent numerical solutions, and the point is made that the initial conditions can not be completely arbitrary. Finally, in order to learn more about the performance of the time-dependent method, a numerical experiment is conducted to examine the unsteady propagation and region of influence of a slight pressure disturbance introduced at a point on the surface of a blunt body.
Author :
Publisher :
Page : 308 pages
File Size : 10,49 MB
Release : 1982
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 616 pages
File Size : 33,59 MB
Release : 1975
Category :
ISBN :
Author :
Publisher :
Page : 758 pages
File Size : 49,28 MB
Release : 1970
Category : Aerodynamics
ISBN :
Author :
Publisher :
Page : 280 pages
File Size : 31,91 MB
Release : 1991
Category : Astronautics
ISBN :
Author : Mamoru Inouye
Publisher :
Page : 26 pages
File Size : 24,19 MB
Release : 1968
Category : Cylinder (Mathematics)
ISBN :
Author :
Publisher :
Page : 1054 pages
File Size : 21,79 MB
Release : 1971
Category : Aerodynamics
ISBN :