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...
Saved in:
| 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 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Wind Tunnel Process Mach Number Prediction Based on Modal, Stage, and Intra-Stages Three-Layer Partitioning
by: Haixuan Yuan, et al.
Published: (2025-05-01) -
Subsonic and Transonic Mach Number Tracking Control Strategy Design and Application in an Intermittent Wind Tunnel
by: Liebo Ma, et al.
Published: (2025-01-01) -
A Multi-Mode Dynamic Fusion Mach Number Prediction Framework
by: Luping Zhao, et al.
Published: (2025-06-01) -
Numerical simulation on the combustion characteristics of scramjet at high Mach number
by: Jiahang Li, et al.
Published: (2025-08-01) -
Effects of Mach Number and Magnetic Fields on Performance of MHDG in Nozzle
by: Li Hao, et al.
Published: (2025-02-01)