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))
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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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