Tables for Numerical Solution of Problems in Compressible Gas Flow With Energy Effects

1948 ◽  
Vol 15 (2) ◽  
pp. 169-175
Author(s):  
Ascher H. Shapiro ◽  
Gilbert M. Edelman

Abstract Tables of functions are given for solving problems in one-dimensional, compressible gas flow when energy effects, as represented by changes in stagnation temperature, are involved. The tables may be used for such typical processes as heat transfer at high gas speeds, combustion, moisture condensation shocks, flame fronts, and detonation waves. The Mach number is the independent argument of the tables, and there is one table for each of six specific-heat ratios, namely, 1.0, 1.1, 1.2, 1.3, 1.4, and 1.67.

2018 ◽  
Vol 1129 ◽  
pp. 012022
Author(s):  
A I Leontiev ◽  
S S Popovich ◽  
Y A Vinogradov ◽  
M M Strongin

2018 ◽  
Vol 482 (1) ◽  
pp. 38-41
Author(s):  
M. Makarova ◽  
◽  
A. Leontiev ◽  
V. Lushik ◽  
◽  
...  

2019 ◽  
Vol 64 (1) ◽  
pp. 44-44
Author(s):  
A. I. Leont’ev ◽  
V. G. Lushchik ◽  
M. S. Makarova

2016 ◽  
Vol 821 ◽  
pp. 70-78 ◽  
Author(s):  
Martin Kyncl ◽  
Jaroslav Pelant

We work with the numerical solution of the turbulent compressible gas flow, and we focus on the numerical solution of these equations, and on the boundary conditions, particularly on the outlet boundary condition with the preference of given mass flow. Usually, the boundary problem is being linearized, or roughly approximated. The inaccuracies implied by these simplifications may be small, but it has a huge impact on the solution in the whole studied area, especially for the non-stationary flow. The boundary condition with the preference of mass flow is sometimes being implemented with the use of some iterative process, guessing the correct values (for the pressure, density, velocity) in order to match the given mass flow through the boundary. In our approach we try to be as exact as possible, using our own original procedures. We follow the exact solution of the initial-value problem for the system of hyperbolic partial differential equations. This complicated problem is modified at the close vicinity of boundary, where the conservation laws are supplied with the additional boundary conditions. We complement the boundary problem suitably, and we show the analysis of the resulting uniquely-solvable modified Riemann problem.The resulting algorithm was coded and used within our own developed code for the solution of the compressible gas flow (the Euler, NS, and RANS equations). The examples show good behaviour of the analyzed boundary condition.


2018 ◽  
Vol 63 (9) ◽  
pp. 371-374 ◽  
Author(s):  
A. I. Leont’ev ◽  
V. G. Lushchik ◽  
M. S. Makarova

1970 ◽  
Vol 13 (8) ◽  
pp. 1261-1270 ◽  
Author(s):  
A.V Luikov ◽  
T.L Perelman ◽  
R.S Levitin ◽  
L.B Gdalevich

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