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Journal of Projectiles, Rockets, Missiles and Guidance >

2013 , Vol. 33 >Issue 5: 115 - 118,122

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2013.05.049

PROJECTILES TECHNOLOGY

Virtual Experiment Platform for Turbofan Engine Overall Performance

  • ZHANG Shiying ,
  • LUO Fangzheng ,
  • HU Yu ,
  • ZHU Jietang
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  • The Second Artillery Engineering University, Xi'an 710025, China

Received date: 2013-02-01

  Online published: 2025-05-26

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Abstract

Due to difficulty, long cycle and high cost of turbofan engine development, a virtual experiment platform for overall performance of turbofan engine was built up. According to the MVC design pattern, the model layer, the experiment control layer and the user interface layer were designed for the virtual experiment platform. Based on LabVIEW virtual instrument development platform, the user interface of virtual experiment platform was designed. Through overall performance virtual experiments of a certain type of turbofan engine, the good visual effect and good expansibility of the platform were verified. Therefore, the virtual experiment platform can be used for design, development and experiment of turbofan engine.

Key words： virtual experiment platform; turbofan engine; overall performance; MVC design pattern; LabVIEW

Cite this article

ZHANG Shiying , LUO Fangzheng , HU Yu , ZHU Jietang . Virtual Experiment Platform for Turbofan Engine Overall Performance[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013 , 33(5) : 115 -118,122 . DOI: 10.15892/j.cnki.djzdxb.2013.05.049

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