Measuring and computational system of TsAGI T-128 transonic wind tunnel

被引：0
|
作者：
V. V. Burov
V. S. Volobuev
S. A. Glazkov
A. R. Gorbushin
E. K. Chumachenko
机构：
[1] Central Aerohydrodynamic Institute (TsAGI),
来源：
Automation and Remote Control | 2011年 / 72卷
关键词：
Mach Number; Remote Control; Wind Tunnel; Test Section; Computational System;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Having been developed at TsAGI, measuring and computational system of T-128 transonic wind tunnel is presented. Structure of the system, as well as basic characteristics of the subsystems used for measuring the aerodynamic loads, pressure distribution and flow parameters are described. Specific features of the system’s software for the given wind tunnel are discussed. Application of the system enables to improve the accuracy of evaluating the aerodynamic characteristics of aircraft models by ten times.
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    Burov, V. V.
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    Chumachenko, E. K.
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  • [5] Influence of T-128 wind tunnel perforated walls on aerodynamic characteristics of reentry vehicles at transonic speed
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    [J]. CEAS SPACE JOURNAL, 2020, 12 (02) : 235 - 246
  • [6] Experimental investigation of the effect of nozzle shape and test section perforation on the stationary and non-stationary characteristics of flow field in the large transonic TsAGI T-128 Wind tunnel
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    [J]. AERONAUTICAL JOURNAL, 2005, 109 (1092): : 75 - 82
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    [J]. Biryukov, V.I., 1600, Royal Aeronautical Society (109):
  • [8] Investigation of the rear support interference on the aerodynamic characteristics of the RRJ-95 model in the T-128 transonic wind tunnel
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    [J]. ICIASF '05 Record: 21st International Congress on Instrumentation in Aerospace Simulation Facilities, 2005, : 76 - 82
  • [9] Experimental Study of Boundary Conditions on the Perforated Walls of Test Sections No. 1 and 2 of T-128 Transonic Wind Tunnel
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  • [10] Determination of the effect due wall interference on the flow around airfoil in the T-128 wind tunnel
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    [J]. THERMOPHYSICS AND AEROMECHANICS, 2023, 30 (03) : 459 - 474
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