MATHEMATICAL MODEL OF THE TSAGI’S TRANSONIC WIND TUNNEL T-106 AS A MACH NUMBER CONTROL OBJECT
In this paper we propose a method of constructing a mathematical model of the TsAGI’s compressor transonic wind tunnel T-106 as a Mach number control object. The mathematical model is sought in the form of a family of linear transfer functions with constant coefficients and delay. Experimental inves...
| Main Authors: | , , |
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| Format: | Article |
| Language: | Russian |
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Moscow State Technical University of Civil Aviation
2016-11-01
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| Series: | Naučnyj Vestnik MGTU GA |
| Subjects: | |
| Online Access: | https://avia.mstuca.ru/jour/article/view/259 |
| Summary: | In this paper we propose a method of constructing a mathematical model of the TsAGI’s compressor transonic wind tunnel T-106 as a Mach number control object. The mathematical model is sought in the form of a family of linear transfer functions with constant coefficients and delay. Experimental investigation of dynamic properties of the wind tunnel T-106 as an object of Mach number control in the subsonic range is provided. The coefficients of the mathematical model of the wind tunnel T-106 is identified on basis the experimental data. |
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| ISSN: | 2079-0619 2542-0119 |