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APPLICATION OF MATHEMATICAL MODELING OF THE AIRCRAFT STRUCTURES STRESS STATE TO OPTIMIZE CORROSION DAMAGE REMOVAL

机译：飞机结构应力状态数学建模的应用优化腐蚀损伤

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D. P. Saidzhanov; V. V. Efimov;
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1. Development and Investigation of Mathematical Models of Thermoelastic Stresses and Strains in Production of Multilayer Structures of Spherical Shape for Aircraft [J] . Russian Aeronautics . 2019,第3期

机译：飞机塑性球形多层结构中热弹性应力和菌株数学模型的发展与研究
2. Mathematic model of the structure diagram for the low-carbon corrosion-resistant steels and its application for design of novel materials [J] . Krivonogov G. S., Kablov E. N. Металлы . 2001,第5期

机译：低碳耐腐蚀钢结构图的数学模型及其在新型材料设计中的应用
3. Mathematic model of the structure diagram for the low-carbon corrosion-resistant steels and its application for design of novel materials [J] . Krivonogov G. S., Kablov E. N. Металлы . 2001,第5期

机译：低碳耐腐蚀钢结构图的数学模型及其对新型材料设计的应用
4. Impact of Pitting Corrosion on the Evolution and Distribution of Fatigue Damage in Aircraft Structures: Model Predictions versus Observations [C] . Robert P. Wei, D. Gary Harlow CORROSION Research Topical Symposium . 2003

机译：蚀腐蚀对飞机结构疲劳损伤进化和分布的影响：模型预测与观察
5. AIRCRAFT MEASUREMENTS AND MATHEMATICAL MODELING OF THE REMOVAL OF GASEOUS AIR POLLUTANTS AT NATURAL AIR-LAND AND AIR-WATER INTERFACES. [D] . DECARIA, ANTHONY JOSEPH. 1981

机译：自然气陆和空气-水界面处气态污染物去除的飞机测量和数学模型。
6. Acrylate-Based Hybrid Sol-Gel Coating for Corrosion Protection of AA7075-T6 in Aircraft Applications: The Effect of Copolymerization Time [O] . Peter Rodič, Romana Cerc Korošec, Barbara Kapun, 2020

机译：基于丙烯酸酯的杂化溶胶-凝胶涂层在飞机应用中对AA7075-T6的腐蚀防护：共聚时间的影响
7. Mathematical model of optimization of annealing regimes by the stress state for heat-sensitive glass elements of structures [O] . O. Hachkevych, M. Hachkevych, A. Torskyy, 2018

机译：用结构热敏玻璃元件应力状态优化退火制度的数学模型
8. Mathematical Modeling of Material Removal Processes for Improved Process Design,Planning,Optimization and Control. [R] . tipnis, v. a. vogel, s. a. 1977

机译：用于改进工艺设计，规划，优化和控制的材料去除过程的数学建模。

APPLICATION OF MATHEMATICAL MODELING OF THE AIRCRAFT STRUCTURES STRESS STATE TO OPTIMIZE CORROSION DAMAGE REMOVAL

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