Репозиторий Самарского университета
Отрывок: 3 of the manual [2]). The three-view general drawing made with CAD system and the list of the main aircraft and engine parameters are given in the end of the project subsection (see the subsection 3.3 of the manual [2]). 11 2.4 Defining the required start thrust-to-weight ratio of the airplane The start thrust-to-weight ratio is the dimensionless value calculated as the ratio of the total static thrust Р0 to the take-off weight of the aircraft. The thrust-to- weight ratio determ...
Полная запись метаданных
| Поле DC | Значение | Язык |
|---|---|---|
| dc.contributor.author | Kozlov D. M. | 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 самолетов | ru |
| dc.date.issued | 2011 | ru |
| dc.identifier | RU/НТБ СГАУ/WALL/629.7.02/C 74-969171 | ru |
| dc.identifier.citation | Conceptual Aircraft Design [Электронный ресурс] : Term Project Guideline / The Ministry of Education and Science of the Russian Federation, Samara State Aerospace University (National Research University) ; [comp. D. M. Kozlov ; tr. G. S. Kancher, A. S. Lyaskin]. - Samara, 2011. - [r=on-line] | ru |
| dc.description.abstract | Труды сотрудников СГАУ(электрон. версия). | ru |
| dc.description.abstract | Ресурс закрыт даже для компьютерной сети университета | ru |
| dc.description.abstract | Goals, tasks, contents and stages of the term project execution, requirements for the term project of the discipline "Conceptual aircraft design" are considered for students of the specialty 160100 “Airplane construction” and for the Masters programme «De | ru |
| dc.description.abstract | Используемые программы: Adobe Acrobat. | ru |
| dc.format.extent | Electronic text (1 файл : 363 Кб) | ru |
| dc.language.iso | rus | ru |
| dc.relation.isformatof | Conceptual Aircraft Design [Электронный ресурс] : Term Project Guideline | ru |
| dc.title | Conceptual Aircraft Design | ru |
| dc.type | Text | ru |
| dc.subject.rugasnti | 55.47 | ru |
| dc.subject.udc | 629.7.02(075) | ru |
| dc.textpart | 3 of the manual [2]). The three-view general drawing made with CAD system and the list of the main aircraft and engine parameters are given in the end of the project subsection (see the subsection 3.3 of the manual [2]). 11 2.4 Defining the required start thrust-to-weight ratio of the airplane The start thrust-to-weight ratio is the dimensionless value calculated as the ratio of the total static thrust Р0 to the take-off weight of the aircraft. The thrust-to- weight ratio determ... | - |
| Располагается в коллекциях: | Методические издания | |
Файлы этого ресурса:
| Файл | Описание | Размер | Формат | |
|---|---|---|---|---|
| Kozlov D. M. Conceptual Aircraft. Term Project.pdf | from 1C | 363.87 kB | Adobe PDF | Просмотреть/Открыть |
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