학술논문

Starting of an axisymmetric convergent-divergent nozzle in a hypersonic flow.
Document Type
Article
Source
Fluid Dynamics. Jul2014, Vol. 49 Issue 4, p557-561. 5p. 2 Diagrams, 3 Graphs.
Subject
*NOZZLES
*FLUID dynamics
*AXIAL flow
*HYPERSONIC flow
*AERODYNAMICS
*AIR flow
*SHOCK waves
*EULER equations
Language
ISSN
0015-4628
Abstract
The starting of an axisymmetric convergent-divergent nozzle, with the result that supersonic flow is formed within almost the entire channel, is modeled, as applied to the hypersonic aerodynamic setup of the Institute of Mechanics of Moscow State University. A successful starting is realized when the nozzle is thrown in a uniform supersonic air flow at a fairly high Mach number. The steady flow structure is studied. It is numerically shown that in the convergent section of the channel there arises an oblique shock wave whose interaction with the nozzle axis leads to the formation of a reflected shock and a curvilinear Mach disk with a region of unsteady subsonic flow in the vicinity of the throat. The mathematical model is based on the two-dimensional Euler equations for axisymmetric gas flows. [ABSTRACT FROM AUTHOR]