Отрывок: 2.4. Defining the stresses of the part elements. Using the design scheme selected previously, the stresses of the crank wall and belts are defined by the formulas given in [2]. The initial data for calculations is shown in the Figure 2.5. The stresses of the belts N13, N23, N12 and the wall T are defined by the formulas (4.1) (4.2) (4.3). 14 Figure 2.5 - The initi...
Полная запись метаданных
Поле DC | Значение | Язык |
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dc.contributor.author | Reznichenko G. A. | ru |
dc.contributor.author | Vyrypaev A. A. | ru |
dc.contributor.author | Kancher G. S. | ru |
dc.contributor.author | Lyaskin A. S. | ru |
dc.contributor.author | The Ministry of Education and Science of the Russian Federation | ru |
dc.contributor.author | Samara State Aerospace University (National Research University) | ru |
dc.coverage.spatial | проектирование детали | ru |
dc.date.issued | 2011 | ru |
dc.identifier | RU/НТБ СГАУ/WALL/629.7.02/D 47-099203 | ru |
dc.identifier.citation | Detail Design of Airframe Part [Электронный ресурс] : Laboratory Work Example / The Ministry of Education and Science of the Russian Federation, Samara State Aerospace University (National Research University) ; [comp. G. A. Reznichenko, A. A. Vyrypaev ; tr. G. S. Kancher, A. S. - Samara, 2011. - [r=on-line] | ru |
dc.description.abstract | Труды сотрудников СГАУ(электрон. версия). | ru |
dc.description.abstract | A method of executing laboratory works in accordance with the discipline of aircraft construction and design is described. A list of normative-technical documentation and reference materials that are needed for executing tasks, as well as examples of the | ru |
dc.description.abstract | Используемые программы: Adobe Acrobat. | ru |
dc.format.extent | Electronic text and graphic data (1 файл : 1,76 Mb) | ru |
dc.language.iso | rus | ru |
dc.relation.isformatof | Detail Design of Airframe Part [Электронный ресурс] : Laboratory Work Example | ru |
dc.title | Detail Design of Airframe Part | ru |
dc.type | Text | ru |
dc.subject.rugasnti | 55.47 | ru |
dc.subject.udc | 629.7.02(075) | ru |
dc.textpart | 2.4. Defining the stresses of the part elements. Using the design scheme selected previously, the stresses of the crank wall and belts are defined by the formulas given in [2]. The initial data for calculations is shown in the Figure 2.5. The stresses of the belts N13, N23, N12 and the wall T are defined by the formulas (4.1) (4.2) (4.3). 14 Figure 2.5 - The initi... | - |
Располагается в коллекциях: | Методические издания |
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Файл | Описание | Размер | Формат | |
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Reznichenko G. A. Detail Design. Laboratory Work.pdf | from 1C | 1.81 MB | Adobe PDF | Просмотреть/Открыть |
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