Modeling of multiphase alumina-loaded jet flow fields

Родионов, А. В.; Plastinin, Yu. A.; Drakes, J. A.; Simmons, Mark; Hiers, Robert S.

doi:10.2514/6.1998-3462

Cited by 12 publications

(12 citation statements)

References 7 publications

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“…The first source is the motor itself. Modeling of non-equilibrium nozzle flow by the NARJ gasdynamic codes 136 results in the OH(X) mole fraction at the nozzle exit X OH ≈3⋅10 -5 for ACS motor and X OH ≈10 -5 for PME. In the near field of the plume 2E-006 -…”

Section: Resonant Scattering Of the Oh(a→x) Radiation In The Plume Flowmentioning

confidence: 99%

“…The single ACS flow gasdynamic characteristics were simulated by the NARJ software package 136 in the axisymmetric approximation. Input parameters for this simulation were 2-D solution of the nozzle flow at the exit.…”

Section: Modeling Of a Single Acs Motor Plume Flow Parametersmentioning

confidence: 99%

“…At the initial stage of the computation the PME nozzle and plume flow (20 meters downstream) was modeled by NARJ 136 Starting surface for the DSMC computation was chosen at 20.18 meters downstream from the PME. This choice was dictated by the necessity to have relatively small collisional mean free path making sure that CFD approach still works here.…”

Section: Computation Of the Gasdynamic Parameters Of The Pme Plume Flmentioning

confidence: 99%

“…Input parameters for the computation are discussed in Section 2.2.1. The nozzle flow was simulated with the use of NARJ software package 136 within the frames of Euler equations. The nozzle flow computation started in the combustion chamber, where the fuel combustion product composition was determined at equilibrium temperature and pressure.…”

Section: Flow Parameters At the Nozzle Exitmentioning

confidence: 99%

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Studying of Atomic and Molecular Interaction Processes in Rarified Hypervelocity Expanding Flows by Methods of Emissive Spectroscopy

Karabadzhak¹

2004

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Section: Resonant Scattering Of the Oh(a→x) Radiation In The Plume Flowmentioning

confidence: 99%

Section: Modeling Of a Single Acs Motor Plume Flow Parametersmentioning

confidence: 99%

Section: Computation Of the Gasdynamic Parameters Of The Pme Plume Flmentioning

confidence: 99%

Section: Flow Parameters At the Nozzle Exitmentioning

confidence: 99%

See 2 more Smart Citations

Studying of Atomic and Molecular Interaction Processes in Rarified Hypervelocity Expanding Flows by Methods of Emissive Spectroscopy

Karabadzhak¹

2004

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“…Under angle of attack, the pure gas effect and gas-solid two-phase flow the effect, numerical simulation using FLUENT software. Based on two dimensional axisymmetric model , N-S equation and turbulence model [1,2,3] , the plume flow field of solid rocket motor is compared with different flight altitude and flight Maher number under the condition of constant attack angle.…”

Section: Introductionmentioning

confidence: 99%

Plume Flow Field Analysis of Solid Rocket Motor

Zhang¹,

Li²

2017

Proceedings of the 3rd Annual International Conference on Mechanics and Mechanical Engineering (MME 2016)

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Abstract. The distribution characteristics of plume field structure of solid rocket motor could great influence on overall design of rocket, design of launch vehicle, materials selection and so on. Therefore, it is necessary to study structure characteristic of plume field of solid rocket engine. In this paper, the numerical simulation of the nozzle and plume flow field rocket motor from air performed using FLUENT software the influence of flying altitude and Ma number on plume flow was analyzed.

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Influence of optical properties of alumina particles on the radiative base heating from solid rocket plume

Lee

Kwon

2019

Advances in Space Research

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Modeling of multiphase alumina-loaded jet flow fields

Cited by 12 publications

References 7 publications

Studying of Atomic and Molecular Interaction Processes in Rarified Hypervelocity Expanding Flows by Methods of Emissive Spectroscopy

Studying of Atomic and Molecular Interaction Processes in Rarified Hypervelocity Expanding Flows by Methods of Emissive Spectroscopy

Plume Flow Field Analysis of Solid Rocket Motor

Influence of optical properties of alumina particles on the radiative base heating from solid rocket plume

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