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
dc.contributor.authorReznichenko G. A.ru
dc.contributor.authorVyrypaev A. A.ru
dc.contributor.authorKancher G. S.ru
dc.contributor.authorLyaskin A. S.ru
dc.contributor.authorThe Ministry of Education and Science of the Russian Federationru
dc.contributor.authorSamara State Aerospace University (National Research University)ru
dc.coverage.spatialпроектирование деталиru
dc.date.issued2011ru
dc.identifierRU/НТБ СГАУ/WALL/629.7.02/D 47-099203ru
dc.identifier.citationDetail 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.abstractТруды сотрудников СГАУ(электрон. версия).ru
dc.description.abstractA 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 theru
dc.description.abstractИспользуемые программы: Adobe Acrobat.ru
dc.format.extentElectronic text and graphic data (1 файл : 1,76 Mb)ru
dc.language.isorusru
dc.relation.isformatofDetail Design of Airframe Part [Электронный ресурс] : Laboratory Work Exampleru
dc.titleDetail Design of Airframe Partru
dc.typeTextru
dc.subject.rugasnti55.47ru
dc.subject.udc629.7.02(075)ru
dc.textpart2.4. 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...-
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