Field of the flow and amplification coefficients in the resonator cavity of a gas-dynamic laser working on the combustion products of kerosene. Two-dimensional calculation and comparison with experiment

1979 ◽  
Vol 15 (1) ◽  
pp. 70-75 ◽  
Author(s):  
M. G. Ktalkherman ◽  
V. A. Levin ◽  
V. M. Mal'kov ◽  
Yu. V. Tunik
Author(s):  
R. A. Peshkov ◽  
D. R. Ismagilov

The paper introduces a mathematical model for calculating the gas-dynamic parameters in the launch container. The model takes into account chemical interactions between the main components of the combustion products, i.e. carbon monoxide and hydrogen, and oxygen. The resulting energy can be used to increase the initiating pulse of the rocket. Within the research, we described the basic requirements for the grid model, and analyzed the accuracy of the results obtained. Furthermore, we compared calculation data of pressure in the launch container with the results of the known method. Findings of research show that the use of two-dimensional and three-dimensional models makes it possible to obtain not only medium-volume gas-dynamic parameters, such as pressure, temperature, density, but also the distribution of these parameters over the computational domain. The developed method of numerical simulation will allow us to estimate the effect of changes in the configuration of the sub-rocket volume and other parameters on the dynamics of the rocket movement without conducting an expensive experiment


1999 ◽  
Author(s):  
John Ward ◽  
Sara A. C. Correia ◽  
João L. V. A. Sousa

Abstract The zone method of radiation analysis has been widely used in mathematical models of a range of industrial heating processes. This paper is thus concerned with the use of a two-dimensional, multi-zone model to predict fuel consumptions, heating rates and load temperatures following the “cold start up” of a gas-fired furnace heating steel bars to a nominal discharge temperature of 1250°C. The model takes into account variations in the flows of the combustion products and in particular examines the influence of the re-circulation of these hot gases within the furnace chamber. The predictions of this complex two-dimensional model are compared with those of a one-dimensional so-called “long furnace model” to illustrate the differences resulting from the use of a more sophisticated multi-zone model.


1996 ◽  
Vol 74 (9-10) ◽  
pp. 603-607 ◽  
Author(s):  
Bernard M. de Dormale

We present a very easy way to take into account exactly the effect of a substrate for a two-dimensional lattice of spheres subject to dipole–dipole interaction. Comparison with experiment shows better agreement than when other dipole treatments are used.


1996 ◽  
Vol 07 (05) ◽  
pp. 717-729 ◽  
Author(s):  
ALEXANDER V. POTAPOV ◽  
CHARLES S. CAMPBELL

This paper describes an extension into three dimensions of an existing two-dimensional technique for simulating brittle solid fracture. The fracture occurs on a simulated solid created by "gluing" together space-filling polyhedral elements with compliant interelement joints. Such a material can be shown to have well-defined elastic properties. However, the "glue" can only support a specified tensile stress and breaks when that stress is exceeded. In this manner, a crack can propagate across the simulated material. A comparison with experiment shows that the simulation can accurately reproduce the size distributions for all fragments with linear dimensions greater than three element sizes.


2000 ◽  
Vol 154-155 ◽  
pp. 66-72 ◽  
Author(s):  
A.V. Gusarov ◽  
A.G. Gnedovets ◽  
I. Smurov

2016 ◽  
Vol 5 (6) ◽  
pp. 30-37
Author(s):  
Дорофеев ◽  
A. Dorofeev ◽  
Бурцев ◽  
I. Burtsev

A system for burning of a destroyed highly toxic substance with formation of a vertical supersonic stream of combustion products moved away to the atmosphere on considerable heights has been considered. A technique and an algorithm for conjugated gas-dynamic and thermodynamic calculation of working processes in two-zonal unit with primary burning using air in a camera similar to the one of a liquid rocket engine, and after-burning in a supersonic flow have been proposed. The technique has been approved on the examples of after-burning mathematical modeling and a parametrical research on combustion completeness influence on composition and properties of products resulting from heptyl combustion in air with after-burning in case of methane supply in the second zone.


2018 ◽  
Vol 44 (12) ◽  
pp. 1163-1166 ◽  
Author(s):  
D. S. Ryashchikov ◽  
N. E. Molevich ◽  
D. I. Zavershinskii

Fluids ◽  
2021 ◽  
Vol 6 (8) ◽  
pp. 278
Author(s):  
Sergey Denisikhin ◽  
Vladislav Emelyanov ◽  
Konstantin Volkov

A numerical simulation of the gas-dynamic processes in the thrust vectorable nozzle of the solid rocket motor is considered. Construction of a geometric model and a generation of computational mesh, and reconstruction of model and mesh at each time step are discussed. Calculations of the flowfield of combustion products in the pre-nozzle chamber and nozzle block are carried out for various angles of nozzle rotation. The distributions of the gas dynamic quantities in the pre-nozzle volume corresponding to the outflow of the combustion products from the cylindrical channel and star-shaped channel are compared, as well as the solutions of the problem obtained with quasi-stationary and unsteady formulations. The effects of the channel shape on the distribution of flow quantities and formation of a vortical flow structure in the nozzle block are discussed.


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