2018Ryuutai Kougaku Bumon Kouenkai kouen rombunshuu/Ryutai Kogaku Bumon Koenkai koen ronbunshuOpen access

Numerical simulation of nozzle flow for design of the devices using supersonic nozzle

Shoma KIMURA, Takashi Imai, Atsushi MATUDA

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Abstract

In this study, as a preliminary step of supersonic nozzle performance prediction for designing the cleaning device with air nozzle, numerical analysis of two-dimensional nozzle flow was conducted. In this paper, CFD analysis of supersonic flow in two dimensions was performed as a preliminary stage. As a result of comparison between theoretical solution and numerical result, agreement between the numerical and the theoretical results can be observed, even though some slight discrepancy appeared. This discrepancy is caused by the fact that the theoretical solution is quasi-one-dimensional, whereas the numerical solution is two-dimensional. In the future, incorporation of subsonic boundary conditions into simulation code should be conducted for the extension of the robustness for the analysis code.

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What this paper is about

In this study, as a preliminary step of supersonic nozzle performance prediction for designing the cleaning device with air nozzle, numerical analysis of two-dimensional nozzle flow was conducted. In this paper, CFD analysis of supersonic flow in two dimensions was performed as a preliminary stage. As a result of comparison between theoretical solution and numerical result, agreement between the numerical and the theoretical results can be observed, even though some slight discrepancy appeared. This discrepancy is caused by the fact that the theoretical solution is quasi-one-dimensional, whereas the numerical solution is two-dimensional. In the future, incorporation of subsonic boundary conditions into simulation code should be conducted for the extension of the robustness for the analysis code.

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Available abstract

In this study, as a preliminary step of supersonic nozzle performance prediction for designing the cleaning device with air nozzle, numerical analysis of two-dimensional nozzle flow was conducted. In this paper, CFD analysis of supersonic flow in two dimensions was performed as a preliminary stage. As a result of comparison between theoretical solution and numerical result, agreement between the numerical and the theoretical results can be observed, even though some slight discrepancy appeared. This discrepancy is caused by the fact that the theoretical solution is quasi-one-dimensional, whereas the numerical solution is two-dimensional. In the future, incorporation of subsonic boundary conditions into simulation code should be conducted for the extension of the robustness for the analysis code.

Key concepts: Nozzle, Supersonic speed, Computer simulation, Mechanics, Choked flow, Robustness (evolution), Numerical analysis, Computational fluid dynamics

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