Мақаланы E-mail арқылы жіберу Static Stability in the Angular Motion of an Aircraft with a Laser-Induced Spike Conical Nozzle
- Авторлар: Sattarov A.1, Sochnev A.1, Bikmuchev A.2
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Мекемелер:
- Tupolev Kazan National Research Technical University
- Gagarin Research and Test Cosmonaut Training Center
- Шығарылым: Том 61, № 2 (2018)
- Беттер: 299-303
- Бөлім: Technical Notes Flight Vehicle Design
- URL: https://journals.rcsi.science/1068-7998/article/view/230543
- DOI: https://doi.org/10.3103/S1068799818020216
- ID: 230543
Дәйексөз келтіру
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Рұқсат берілді
Тек жазылушылар үшін
Аннотация
The location of the center of mass closer to the source of radiation during rectilinear accelerated motion of an aircraft in the absence of gravity and drag forces provides stability of the angular motion. The proposed scheme was analyzed on the basis of the Lagrange–Dirichlet theorem.
Негізгі сөздер
Авторлар туралы
A. Sattarov
Tupolev Kazan National Research Technical University
Email: sochnev.aleksandr@inbox.ru
Ресей, ul. Karla Marksa 10, Kazan, 420111
A. Sochnev
Tupolev Kazan National Research Technical University
Хат алмасуға жауапты Автор.
Email: sochnev.aleksandr@inbox.ru
Ресей, ul. Karla Marksa 10, Kazan, 420111
A. Bikmuchev
Gagarin Research and Test Cosmonaut Training Center
Email: sochnev.aleksandr@inbox.ru
Ресей, Zvesdnyi gorodok, Moskovskaya oblast, 141160
