Study of Procedure Errors of the Vortex Air Data System of a Subsonic Aircraft


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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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E. Efremova

Tupolev Kazan National Research Technical University

Email: w-soldatkin@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111

V. Soldatkin

Tupolev Kazan National Research Technical University

编辑信件的主要联系方式.
Email: w-soldatkin@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111

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