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...

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Main Authors: K. D. Bukharov, V. V. Petronevich, P. V. Savin
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-11-01
Series:Научный вестник МГТУ ГА
Subjects:
Online Access:https://avia.mstuca.ru/jour/article/view/259
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author K. D. Bukharov
V. V. Petronevich
P. V. Savin
author_facet K. D. Bukharov
V. V. Petronevich
P. V. Savin
author_sort K. D. Bukharov
collection DOAJ
description 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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institution DOAJ
issn 2079-0619
2542-0119
language Russian
publishDate 2016-11-01
publisher Moscow State Technical University of Civil Aviation
record_format Article
series Научный вестник МГТУ ГА
spelling doaj-art-9aa560b2e9ad4bdea0ab5a0dab08df5f2025-08-20T02:59:49ZrusMoscow State Technical University of Civil AviationНаучный вестник МГТУ ГА2079-06192542-01192016-11-01223109114259MATHEMATICAL MODEL OF THE TSAGI’S TRANSONIC WIND TUNNEL T-106 AS A MACH NUMBER CONTROL OBJECTK. D. Bukharov0V. V. Petronevich1P. V. Savin2ЦАГИФАЛТ МФТИЦАГИIn 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.https://avia.mstuca.ru/jour/article/view/259mathematical modelmach numberwind tunnel
spellingShingle K. D. Bukharov
V. V. Petronevich
P. V. Savin
MATHEMATICAL MODEL OF THE TSAGI’S TRANSONIC WIND TUNNEL T-106 AS A MACH NUMBER CONTROL OBJECT
Научный вестник МГТУ ГА
mathematical model
mach number
wind tunnel
title MATHEMATICAL MODEL OF THE TSAGI’S TRANSONIC WIND TUNNEL T-106 AS A MACH NUMBER CONTROL OBJECT
title_full MATHEMATICAL MODEL OF THE TSAGI’S TRANSONIC WIND TUNNEL T-106 AS A MACH NUMBER CONTROL OBJECT
title_fullStr MATHEMATICAL MODEL OF THE TSAGI’S TRANSONIC WIND TUNNEL T-106 AS A MACH NUMBER CONTROL OBJECT
title_full_unstemmed MATHEMATICAL MODEL OF THE TSAGI’S TRANSONIC WIND TUNNEL T-106 AS A MACH NUMBER CONTROL OBJECT
title_short MATHEMATICAL MODEL OF THE TSAGI’S TRANSONIC WIND TUNNEL T-106 AS A MACH NUMBER CONTROL OBJECT
title_sort mathematical model of the tsagi s transonic wind tunnel t 106 as a mach number control object
topic mathematical model
mach number
wind tunnel
url https://avia.mstuca.ru/jour/article/view/259
work_keys_str_mv AT kdbukharov mathematicalmodelofthetsagistransonicwindtunnelt106asamachnumbercontrolobject
AT vvpetronevich mathematicalmodelofthetsagistransonicwindtunnelt106asamachnumbercontrolobject
AT pvsavin mathematicalmodelofthetsagistransonicwindtunnelt106asamachnumbercontrolobject