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TAS25/100C-3B Computer Controlled Supersonic Wind Tunnel (Three Blowers)
革新的なシステム
The Computer Controlled Supersonic Wind Tunnel (Three Blowers), "TAS25/100C-3B", is an open wind tunnel for the study of theaerodynamic properties of different drag bodies subject to subsonic and supersonic flows.
関連ニュース
概要
The Computer Controlled Supersonic Wind Tunnel (Three Blowers), "TAS25/100C-3B", is an open wind tunnel for the study of theaerodynamic properties of different drag bodies subject to subsonic and supersonic flows.
Airflows through three vacuum pumps or blowers incorporating a computer controlled powerregulator, located on the discharge side of the tunnel. The air enters the tunnel through anozzle, which has a flow rectifier where the fluid is accelerated. Then, the transparent workingsection is located, which consists of a section where the resistance models are mounted, and theaccelerated air flows around these models. The models included have different forms: rocket,projectile, wedges of different slops and double wedge with different inclinations.
There are three different upper profiles of the working section to generate different velocities upto two times the speed of sound (2 Mach).
The optional "TAS25/100-SO" accessory, an optical Schlieren system, allows you to directlyobserve and photograph the supersonic flow and shock fronts formed around the aerodynamicmodels, thus enabling a greater number of experiments.
This Computer Controlled Unit is supplied with the EDIBON Computer Control System (SCADA), and includes: The unit itself + aControl Interface Box + a Data Acquisition Board + Computer Control, Data Acquisition and Data Management Software Packages, forcontrolling the process and all parameters involved in the process.
演習と指導の慣行
マニュアルに含まれるガイド付き実習
- Pressure distribution in subsonic and supersonic flows.
- Calculation of the air velocity inside a supersonic wind tunnel.
- Comparison between experimental and theoretical pressureprofile.
- Pressure distribution in a two-dimensional model under subsonicand supersonic flows.
- Influence of the attack angle on the forces exerted on a doublewedge model.
- Shock wave display (required TAS25/100-SO accessory).
- Determination of Mach number from the shock wave angle(required TAS25/100-SO accessory).
- Experimental testing of the relationship between corner angle,Mach number and shock wave angle (required TAS25/100-SOaccessory).
より実用的な練習をして、ユニットを完成させる
- Many students view results simultaneously.To view all results in real time in the classroom by means of aprojector or an electronic whiteboard.
- Open Control, Multicontrol and Real Time Control.This unit allows intrinsically and/or extrinsically to change thespan, gains, proportional, integral, derivative parameters, etc,in real time.
- The Computer Control System with SCADA allows a realindustrial simulation.
- This unit is totally safe as uses mechanical, electrical/electronic,and software safety devices.
- This unit can be used for doing applied research.
- This unit can be used for giving training courses to Industrieseven to other Technical Education Institutions.
- Control of the TAS25/100C-3B unit process through the controlinterface box without the computer.
- Visualization of all the sensors values used in the TAS25/100C-3B unit process.
- Several other exercises can be done and designed by the user.
補完的な機器
8.6.- 空気力学
TAS25/100C
The Computer Controlled Supersonic Wind Tunnel, "TAS25/100C", is an open wind tunnel for the study of the aerodynamic properties of different drag bodies subject to subsonic and supersonic flows. Air flows through a vacuum pump or blower...
8.6.- 空気力学
TA50/250C
コンピューター制御エアロダイナミックトンネル, 50x250mm
The Computer Controlled Aerodynamic Tunnel, 50 x 250 mm, "TA50/250C", is a wind tunnel designed to study subsonic aerodynamics in a tunnel in open circuit and with incompressible subsonic flow. Air is drawn by a variable speed fan, computer...
8.6.- 空気力学
TA50/250
エアロダイナミックトンネル,50x250mm
The Aerodynamic Tunnel, 50 x 250 mm, "TA50/250", is a wind tunnel designed to study subsonic aerodynamics in a tunnel in open circuit and with incompressible subsonic flow. Air is drawn by a variable speed fan located at the discharge end of the...
8.6.- 空気力学
TA300/300C
Computer Controlled Aerodynamic Tunnel, 300X300 mm
The Computer Controlled Aerodynamic Tunnel, 300 x 300 mm, "TA300/300C", is a wind tunnel designed to study subsonic aerodynamics in a tunnel in open circuit and with incompressible subsonic flow. Air is drawn by a variable speed fan, computer...
8.6.- 空気力学
TA300/300
Aerodynamic Tunnel, 300X300 mm
The Aerodynamic Tunnel, 300 x 300 mm, "TA300/300", is a wind tunnel designed to study subsonic aerodynamics in a tunnel in open circuit and with incompressible subsonic flow. Air is drawn by a variable speed fan located at the discharge end of the...
8.6.- 空気力学
TA610/915C
Computer Controlled Aerodynamic Tunnel, 610X915 mm
Aerodynamics is the part of fluid mechanics that studies the motion of gases and the forces or reactions to which the bodies they interact with are subjected. Aerodynamics is not only important by itself but also as a complement to aeronautics....
8.6.- 空気力学
TA1000/1000C
Computer Controlled Aerodynamic Tunnel, 1000X1000 mm
Aerodynamics is the part of fluid mechanics that studies the motion of gases and the forces or reactions to which the bodies they interact with are subjected. Aerodynamics is not only important by itself but also as a complement to aeronautics....
8.6.- 空気力学
TA1200/1200C
コンピューター制御エアロダイナミックトンネル,1200x1200mm
Aerodynamics is the part of fluid mechanics that studies the motion of gases and the forces or reactions to which the bodies they interact with are subjected. Aerodynamics is not only important by itself but also as a complement to aeronautics....
8.6.- 空気力学
TACL2000/2000C
Computer Controlled Closed Aerodynamic Tunnel, 2000X2000 mm
Aerodynamics is the part of fluid mechanics that studies the motion of gases and the forces or reactions to which the bodies they interact with are subjected. Aerodynamics is not only important by itself but also as a complement to aeronautics....
8.4.- 流れの可視化
TAVF180/100
Flow Visualization Aerodynamic Tunnel
The Flow Visualization Aerodynamic Tunnel, "TAVF180/100", consists of a vertical conduction in which an upward flow of air and smoke is induced, which passes through different models allowing to study the behavior of the flow around it. Thus it is...
8.6.- 空気力学
TADV225/450
Wind Tunnel Flight Demonstration Unit
The Aerodynamic Tunnel for Flight Demonstration, "TADV225/450", consists of an open wind tunnel in whose working section the model of an aircraft with fixed wings is located. The aircraft is piloted by the user using controls similar to those of a...
8.6.- 空気力学
ATBB
Aerodynamic Testing Bench
The Aerodynamic Testing Bench, "ATBB", has two main components: a radial fan with speed control and a working section where the different accessories for the tests are fixed. The radial blower impels the air through an air intake pipe to a...
品質
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アフターサービス
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