Mathematical Model of Fluid Flow in Rocket Fuel System

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Klyuev Nikolay
Klyuev Nikolay
α Samara State Technical University Samara State Technical University

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Mathematical Model of Fluid Flow in Rocket Fuel System

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Abstract

The article reviews mathematical model of liquid flow in metering system of fuel tank of rocket. The control system contains one horizontal and two vertical channels. Vertical channel has sensors for fixing free surface level of fluid in the channel. When the level of fuel reaches the sensor, it is activated, and the signal comes to the control system. As a result, fuel consumption is changing. Fuel level in the tank is determined on the basis of the fuel level in the channel. It is known that in the course of fuel consumption, surface free levels in the channel and in the tank do not match. The task is described by unsteady-state equation of motion. Viscous incompressible liquid model is used. The solution of the differential equation was performed numerically. Measurement error of liquid level in the fuel tank has been determined. The study proposes engineering solution to avoid the measurement error.

References

15 Cites in Article
  1. Kohei Ozawa,Koki Kitagawa,Toru Shimada (2015). Flight Performance Simulations of Vertical Launched Sounding Rockets Using Altering-Intensity Swirling-Oxidizer-Flow-Type Hybrid Motors.
  2. N Slezkin (1955). Dynamics of viscous incompressible fluid.
  3. L Loytsyansky (1970). Visual Resources.
  4. D Popov (1982). Unsteady hydromechanical processes.
  5. Zhan Liu,Quanke Feng (2016). Numerical analysis of gas pulsation attenuation characteristics of a perforated tube in a reciprocating compressor piping system.
  6. Chao Wang,Jian-Dong Yang (2015). Water Hammer Simulation Using Explicit–Implicit Coupling Methods.
  7. M Abdulkadir,V Hernandez-Perez,I Lowndes,B Azzopardi,E Sam-Mbomah (2016). Experimental study of the hydrodynamic behaviour of slug flow in a horizontal pipe.
  8. Xinhui Si,Mingyang Pan,Liancun Zheng,Jianhui Zhou,Lin Li (2016). The solutions for the flow of micropolar fluid through an expanding or contracting channel with porous walls.
  9. Ali Majd,Ahmad Ahmadi,Alireza Keramat (2016). Investigation of Non-Newtonian Fluid Effects during Transient Flows in a Pipeline.
  10. A Avramenko,A Tyrinov,I Shevchuk (2015). An analytical and numerical study on the start-up flow of slightly rarefied gases in a parallel-plate channel and a pipe.
  11. A Noorani,P Schlatter (2015). Evidence of sublaminar drag naturally occurring in a curved pipe.
  12. J Behbahani,A Dahaghin,Z Behbahani (2015). Modeling of Flow of Crude Oil in a Circular Pipe Driven by Periodic Pressure Variations // Energy Sources.
  13. Mariana Simão,Jesus Mora-Rodriguez,Helena Ramos (2015). Mechanical Interaction in Pressurized Pipe Systems: Experiments and Numerical Models.
  14. I Korade,Z Virag,M Šavar (2014). Numerical simulation of one-dimensional flow in elastic and viscoelastic branching tube // 11th World Congress on Computational Mechanics.
  15. S Balta,F Smith (2016). Inviscid and low-viscosity flows in multi-branching and reconnecting networks.

Funding

No external funding was declared for this work.

Conflict of Interest

The authors declare no conflict of interest.

Ethical Approval

No ethics committee approval was required for this article type.

Data Availability

Not applicable for this article.

How to Cite This Article

Klyuev Nikolay. 2017. \u201cMathematical Model of Fluid Flow in Rocket Fuel System\u201d. Global Journal of Research in Engineering - D: Aerospace Science GJRE-D Volume 17 (GJRE Volume 17 Issue D2): .

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Journal Specifications

Crossref Journal DOI 10.17406/gjre

Print ISSN 0975-5861

e-ISSN 2249-4596

Keywords
Classification
GJRE-D Classification: FOR Code: 090199
Version of record

v1.2

Issue date

December 27, 2017

Language
en
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The article reviews mathematical model of liquid flow in metering system of fuel tank of rocket. The control system contains one horizontal and two vertical channels. Vertical channel has sensors for fixing free surface level of fluid in the channel. When the level of fuel reaches the sensor, it is activated, and the signal comes to the control system. As a result, fuel consumption is changing. Fuel level in the tank is determined on the basis of the fuel level in the channel. It is known that in the course of fuel consumption, surface free levels in the channel and in the tank do not match. The task is described by unsteady-state equation of motion. Viscous incompressible liquid model is used. The solution of the differential equation was performed numerically. Measurement error of liquid level in the fuel tank has been determined. The study proposes engineering solution to avoid the measurement error.

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Mathematical Model of Fluid Flow in Rocket Fuel System

Klyuev Nikolay
Klyuev Nikolay Samara State Technical University

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