Study of Procedure Errors of the Vortex Air Data System of a Subsonic Aircraft
- Autores: Efremova E.S.1, Soldatkin V.V.1
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Afiliações:
- Tupolev Kazan National Research Technical University
- Edição: Volume 61, Nº 4 (2018)
- Páginas: 613-619
- Seção: Aircraft Instruments and Instrumentation Computer Complexes
- URL: https://journals.rcsi.science/1068-7998/article/view/230733
- DOI: https://doi.org/10.3103/S1068799818040165
- ID: 230733
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Resumo
The features of design and structural-functional scheme of the vortex air data system for a subsonic aircraft are considered. Mathematical models are revealed and procedure aerodynamic errors of the system measuring channels are quantitatively estimated.
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Sobre autores
E. Efremova
Tupolev Kazan National Research Technical University
Email: w-soldatkin@mail.ru
Rússia, ul. Karla Marksa 10, Kazan, 420111
V. Soldatkin
Tupolev Kazan National Research Technical University
Autor responsável pela correspondência
Email: w-soldatkin@mail.ru
Rússia, ul. Karla Marksa 10, Kazan, 420111
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