Abstract

With the development of large-thrust liquid rocket engines, the behavior of liquid in supercritical conditions arouses increasing public interest. Due to the high pressure and temperature of the combustion chamber, fuel reaches its critical point much more easily, and enters supercritical conditions. Due to the drastic changes in the physical properties of the fluid near the critical point, it is usually difficult to simulate the fluid motion using traditional computational fluid dynamic methods; but molecular dynamics (MD) can simulate fluid motion at the molecular level. In view of the engineering application, the physical properties of a binary system consisting of argon and nitrogen, and the stability of subcritical jets sprayed into supercritical environment, has been studied here using the MD method. First, the molecular dynamic simulation of the equation of state (EOS) of the mixture was put forward. Four conditions, with different mixing ratios of nitrogen, were designed. The results showed that the mixing ratio of nitrogen noticeably affected the results; these results were compared with the Soave-Redich-Kwong (SRK) EOS. Second, a simulation was conducted of subcritical nitrogen jet sprayed into a supercritical argon environment. After analyzing the results, the jet density and temperature distributions were obtained and the disturbance growth rate of the shear layer was analyzed.

Highlights

  • The rapid development of aerospace technology and large-thrust liquid propellant rocket engines (LPRE) has brought with it increasing public attention

  • The molecular dynamics simulation of a methods was constructed and the calculating properties compared with theoretical results calculated nitrogen jet was performed at different conditions

  • Zhang simulated the thermodynamic properties of nitrogen using molecular dynamics (MD) and compared the results with SRK equation of state (EOS) [19]

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Summary

Introduction

The rapid development of aerospace technology and large-thrust liquid propellant rocket engines (LPRE) has brought with it increasing public attention. Due to the high pressure and temperature in the combustion chamber, the jet of a fuel reaches a critical point and transforms into a supercritical state. Unlike the traditional subcritical jet, properties of the jet near the critical point are much more complicated. The surface of the jet breaks up and numbers of droplets can be observed. As the temperature and pressure increases, the environment enters into a supercritical state, where it can be observed that the interface between gas and liquid is replaced by mixing turbulence. Traditional of solving subcritical problems are basedfrom the continuum linear gradient theory [4].Navier-Stokes. Traditional methods of solving jet problems are based on the on the regime and equations, which subcritical do not explain supercritical continuum regime and Navier-Stokes equations, which do not explain supercritical phenomena

Shadowgraphs of coaxial liquid nitrogen injection helium co-flow helium
Molecular Dynamics Model
Left the simulation
Force Routine
Leonard-Jones
Spatial Growth Rate
Equation of State
7.23, Results of dynamics nitrogen compared with
Results ofofmolecular molecular with
11. The temperature and pressure of the nitrogen jet were
Spatial
15. Contour of nitrogen
10.5 REVIEW
Conclusion
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