Static Stability in the Angular Motion of an Aircraft with a Laser-Induced Spike Conical Nozzle
- 作者: Sattarov A.1, Sochnev A.1, Bikmuchev A.2
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隶属关系:
- Tupolev Kazan National Research Technical University
- Gagarin Research and Test Cosmonaut Training Center
- 期: 卷 61, 编号 2 (2018)
- 页面: 299-303
- 栏目: Technical Notes Flight Vehicle Design
- URL: https://journals.rcsi.science/1068-7998/article/view/230543
- DOI: https://doi.org/10.3103/S1068799818020216
- ID: 230543
如何引用文章
详细
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.
作者简介
A. Sattarov
Tupolev Kazan National Research Technical University
Email: sochnev.aleksandr@inbox.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111
A. Sochnev
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: sochnev.aleksandr@inbox.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111
A. Bikmuchev
Gagarin Research and Test Cosmonaut Training Center
Email: sochnev.aleksandr@inbox.ru
俄罗斯联邦, Zvesdnyi gorodok, Moskovskaya oblast, 141160