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The set of mathematical modelling tools and test facility concept for сrash-resistant fuel system

Grachev Sergej Vasil'evich  (Moscow Aviation Institute (National Research University))

Smagin Denis Igorevich  (Moscow Aviation Institute (National Research University))

Savel’ev Roman Sergeevich  (Moscow Aviation Institute (National Research University))

The article considers the set of mathematical modelling tools and test facility concept for crash-resistant fuel system. The main requirements for advanced crash-resistant fuel system are based on aviation aircraft certification rules. A distinctive feature of the concept discussed in this article is a comprehensive development for creating mathematical modeling tools and test facility. The solution includes the complete digital model of the tested system and full-scale test facility that includes rotating platforms for simulation different spatial helicopter positions and equipment complex. The article presents description of full-scale test facility key elements and mathematical model units. This solution makes it possible to ensure combined full-scale and digital testing of crash-resistant fuel system at the all stages of helicopter life-cycle.

Keywords:Mathematical model, сrash-resistant fuel system, test facility, one-dimensional model, three-dimensional model, helicopter.

 

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Citation link:
Grachev S. V., Smagin D. I., Savel’ev R. S. The set of mathematical modelling tools and test facility concept for сrash-resistant fuel system // Современная наука: актуальные проблемы теории и практики. Серия: Естественные и Технические Науки. -2020. -№10. -С. 56-60 DOI 10.37882/2223-2966.2020.10.10
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