Extension of the method of characteristics for simulation of solute transport in three dimensions

The equations of the steady state, compressible inviscid gaseous flow are linearized in a form suitable for application to nozzles of the Laval type. The procedure in the supersonic phase is verified by comparing solutions so obtained with those derived by the method of characteristics in two and three dimensions. Likewise, the solutions in the transonic phase are com pared with those obtained by other investigators. The linearized equation is then used to investigate the nat re of non-symmetric flow in rocket nozzles. It is found that if the flow from the combustion chamber into the nozzle is non-symmetric, the magnitude and direction of the turning couple produced by the emergent jet is dependent on the profile of the nozzle and it is possible to design profiles such that the turning couples or lateral forces are zero. The optimum nozzle so designed is independent of the pressure and also of the magnitude of the non-symmetry of the entry flow. The formulae by which they are obtained have been checked by extensive static and projection tests with simulated rocket test vehicles which are described in this paper.


Soil Research ◽  
1984 ◽  
Vol 22 (1) ◽  
pp. 31 ◽  
Author(s):  
CJ Barnes ◽  
LAG Aylmore

The method of characteristics is used to analyse multi-species solute movement through a non-linearly reactive soil taking dispersion into account. Both ionic and non-ionic solutes are considered, and it is shown that the shape of a solute front depends on the shape of the adsorption isotherms. At large times, overall solute movement is effected by a series of solute fronts moving independently. The composition of each front, and hence individual solute concentrations within the front, are determined by the degree of competition reflected in the adsorption isotherms. Varying water contents are considered explicitly, although the detailed analysis is restricted to uniform water contents for simplicity.


1956 ◽  
Vol 1 (4) ◽  
pp. 409-423 ◽  
Author(s):  
Maurice Holt

The method of characteristics for steady supersonic flow problems in three dimensions, due to Coburn & Dolph (1949), is extended so that flow with shocks and entropy changes may be treated. Equations of motion based on Coburn & Dolph's characteristic coordinate system are derived and a scheme is described for solving these by finite differences.A linearized method of characteristics is developed for calculating perturbations of a given three-dimensional field of flow. This is a generalization of the method evolved by Ferri (1952) for perturbations of plane flow and conical flow.


1983 ◽  
Vol 4 (4) ◽  
pp. 277-287 ◽  
Author(s):  
D. A. Barry ◽  
J. -Y. Parlange ◽  
P. G. Saffigna ◽  
C. W. Rose

1978 ◽  
Vol 100 (4) ◽  
pp. 690-696 ◽  
Author(s):  
A. D. Anderson ◽  
T. J. Dahm

Solutions of the two-dimensional, unsteady integral momentum equation are obtained via the method of characteristics for two limiting modes of light gas launcher operation, the “constant base pressure gun” and the “simple wave gun”. Example predictions of boundary layer thickness and heat transfer are presented for a particular 1 in. hydrogen gun operated in each of these modes. Results for the constant base pressure gun are also presented in an approximate, more general form.


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