DYNAMICS OF PROGRESS AND APPLICATION OF MATHEMATICAL MODELS AT DIFFERENT STAGES OF GAS TURBINE ENGINE DEVELOPMENT

I. A. Krivosheyev; D. A. Akhmedzyanov; O. N. Ivanova

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DYNAMICS OF PROGRESS AND APPLICATION OF MATHEMATICAL MODELS AT DIFFERENT STAGES OF GAS TURBINE ENGINE DEVELOPMENT

机译：燃气轮机发动机不同发展阶段的动力学模型及其应用

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We consider special features in the application of mathematical models at different stages of aircraft engine development (design and adjustment). It is shown that when systems of multilevel multiaspect network simulation are used, a model can dynamically progress during engine development as a design tree. We discuss a problem of model equivalence: its evaluation, requirements at different stages of development; we propose a mechanism for considering stochasticity and control of model equivalence.

机译：我们考虑在飞机发动机开发的不同阶段（设计和调整）的数学模型应用中的特殊功能。结果表明，当使用多级多方面网络仿真系统时，模型可以在引擎开发过程中动态发展为设计树。我们讨论了模型对等的问题：模型的评估，不同开发阶段的需求;我们提出了一种考虑模型的随机性和模型等效性的控制机制。

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《Russian Aeronautics》 |2003年第3期|共4页
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I. A. Krivosheyev; D. A. Akhmedzyanov; O. N. Ivanova;
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中图分类航空;
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1. DYNAMICS OF PROGRESS AND APPLICATION OF MATHEMATICAL MODELS AT DIFFERENT STAGES OF GAS TURBINE ENGINE DEVELOPMENT [J] . I. A. Krivosheyev, D. A. Akhmedzyanov, O. N. Ivanova Russian Aeronautics . 2003,第3期

机译：燃气轮机发动机不同发展阶段的动力学模型及其应用
2. Dynamics of Progress and Application of Mathematical Models at Different Stages of Gas Turbine Engine Development [J] . I.A. KRIVOSHEYEV, D.A. AKHMETZYANOV, O.N. IVANOVA Известия　Высших　учебных　заведений: Авиационная　техника . 2003,第3期

机译：燃气轮机开发不同阶段的数学模型进展及应用动力学
3. Dynamics of Progress and Application of Mathematical Models at Different Stages of Gas Turbine Engine Development [J] . I.A. KRIVOSHEYEV, D.A. AKHMETZYANOV, O.N. IVANOVA Известия　Высших　учебных　заведений: Авиационная　техника . 2003,第3期

机译：进步的动力，并在燃气涡轮发动机不同发展阶段的数学模型中的应用
4. Mathematical Modeling and Optimization of Flow Structure in Stage of Francis Turbine of Micro Gas Turbine Power Plant [C] . A.L. Kartashev, S.D. Vaulin, M.A. Kartasheva, International Conference of Numerical Analysis and Applied Mathematics . 2016

机译：微型燃气轮机发电厂竞技汽轮机舞台流动结构的数学建模与优化
5. An experimental investigation of clocking effects on turbine aerodynamics using a modern 3-D one and one-half stage high pressure turbine for code verification and flow model development. [D] . Haldeman, Charles Waldo, IV. 2003

机译：使用现代的3-D一分半高压涡轮进行代码验证和流模型开发的时钟对涡轮空气动力学影响的实验研究。
6. Application of a Mathematical Model to Describe the Effects of Chlorpyrifos on Caenorhabditis elegans Development [O] . Windy A. Boyd, Marjolein V. Smith, Grace E. Kissling, 2009

机译：数学模型描述毒死rif对秀丽隐杆线虫发育的影响
7. ATEC: The Aerodynamic Turbine Engine Code for the Analysis of Transient and Dynamic Gas Turbine Engine System Operations: Part 1 — Model Development [O] . Doug Garrard 1996

机译：ATEC：用于分析瞬态和动态燃气涡轮发动机系统操作的空气动力学涡轮发动机代码：第1部分 - 模型开发

DYNAMICS OF PROGRESS AND APPLICATION OF MATHEMATICAL MODELS AT DIFFERENT STAGES OF GAS TURBINE ENGINE DEVELOPMENT

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