Are you a teacher or do you work as an engineering researcher? EDIBON offers courses for teachers and #research staff. Take a look at the course of Fluid Mechanics and learn about #fluids properties. #DiscoverEdibon #Engineering.
TAS25/100C Computer Controlled Supersonic Wind Tunnel
創新系統
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.
扩展
相關新聞
一般說明
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 incorporating a computer controlled power regulator, located on the discharge side of the tunnel.
The air enters the tunnel through a nozzle, which has a flow rectifier where the fluid is accelerated. Then, the transparent working section is located, which consists of a section where the resistance models are mounted, and the accelerated 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 up to two times the speed of sound (2 Mach).
The optional "TAS25/100-SO" accessory, an optical Schlieren system, allows you to directly observe and photograph the supersonic flow and shock fronts formed around the aerodynamic models, 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 + a Control Interface Box + a Data Acquisition Board + Computer Control, Data Acquisition and Data Management Software Packages, for controlling the process and all parameters involved in the process.
練習和指導練習
手册中包含的指导实践练习
- Pressure distribution in subsonic and supersonic flows.
- Calculation of the air velocity inside a supersonic wind tunnel.
- Comparison between experimental and theoretical pressure profile.
- Pressure distribution in a two-dimensional model under subsonic and supersonic flows.
- Influence of the attack angle on the forces exerted on a double wedge 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-SO accessory).
与该单位进行更多实际操作
- Many students view results simultaneously. To view all results in real time in the classroom by means of a projector or an electronic whiteboard.
- Open Control, Multicontrol and Real Time Control. This unit allows intrinsically and/or extrinsically to change the span, gains, proportional, integral, derivative parameters, etc, in real time.
- The Computer Control System with SCADA allows a real industrial 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 Industries even to other Technical Education Institutions.
- Control of the TAS25/100C unit process through the control interface box without the computer.
- Visualization of all the sensors values used in the TAS25/100C unit process.
- Several other exercises can be done and designed by the user.
可用的类似设备
8.6.- 空气动力学
TA50/250
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.- 空气动力学
TA50/250C
Computer Controlled Aerodynamic Tunnel, 50 x 250 mm
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.- 空气动力学
TA300/300C
Computer Controlled Aerodynamic Tunnel, 300 x 300 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.- 空气动力学
TA300/300
Aerodynamic Tunnel, 300 x 300 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.- 空气动力学
TAS25/100C-3B
Computer Controlled Supersonic Wind Tunnel (Three Blowers)
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...
配套设备
8.6.- 空气动力学
TAS25/100C-3B
Computer Controlled Supersonic Wind Tunnel (Three Blowers)
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...
8.6.- 空气动力学
TA50/250C
Computer Controlled Aerodynamic Tunnel, 50 x 250 mm
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.- 空气动力学
TA50/250
Aerodynamic Tunnel, 50 x 250 mm
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.- 空气动力学
TA300/300C
Computer Controlled Aerodynamic Tunnel, 300 x 300 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.- 空气动力学
TA300/300
Aerodynamic Tunnel, 300 x 300 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.- 空气动力学
TA1200/1200
Computer Controlled Aerodynamic Tunnel, 1200x1200 mm
The Computer Controlled Aerodynamic Tunnel, 1200x1200 mm. section for testing "TA1200/1200", with these main characteristics:Adequate size for demonstration tests and teaching.Suitable for three-dimensional models.Test chamber built with...
8.4.- 流可视化
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.- 空气动力学
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.- 空气动力学
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...
質量

售後服務
