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.
0
Sélection
/
Vide
Votre sélection
Il n'y a plus d'articles dans votre sélection
TAS25/100C-3B Soufflerie Supersonique Contrôlée par Ordinateur (Trois Compresseurs)
SYSTEMES INNOVANTS
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.
NOUVELLES LIÉES
Description Générale
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.
Des exercices et pratiques guidées
EXERCICES GUIDÉS INCLUS DANS LE MANUEL
- 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).
PLUS D'EXERCICES PRATIQUES À EFFECTUER AVEC CETTE ÉQUIPEMENT
- 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.
EQUIPEMENT COMPLEMENTAIRE
8.6.- AÉRODYNAMIQUE
TAS25/100C
La Soufflerie Supersonique Contrôlée par Ordinateur (PC), "TAS25/100C", est une soufflerie ouverte pour l'étude des propriétés aérodynamiques de différents corps de traînée exposés aux écoulements subsoniques et supersoniques. La circulation de...
8.6.- AÉRODYNAMIQUE
TA50/250C
Tunnel Aérodynamique, 50x250 mm, Contrôlé par Ordinateur (PC)
Le Tunnel Aérodynamique, 50x250 mm, Contrôlé par Ordinateur (PC), "TA50/250C", est une soufflerie conçue pour étudier l'aérodynamique subsonique dans un tunnel en circuit ouvert et avec un écoulement subsonique incompressible. L'air est aspiré par...
8.6.- AÉRODYNAMIQUE
TA50/250
Tunnel Aérodynamique, 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.- AÉRODYNAMIQUE
TA300/300C
Tunnel Aérodynamique, 300 x 300 mm, Contrôlé par Ordinateur (PC)
Le Tunnel Aérodynamique, 300 x 300 mm, Contrôlé par Ordinateur (PC) , 300 x 300 mm, "TA300/300C", est une soufflerie conçue pour étudier l’aérodynamique subsonique dans un tunnel en boucle ouverte et avec un flux subsonique incompressible. L’air...
8.6.- AÉRODYNAMIQUE
TA300/300
Tunnel aérodynamique, 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.- AÉRODYNAMIQUE
TA610/915C
Tunnel Aérodynamique, 610X915 mm, Contrôlé par Ordinateur (PC)
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.- AÉRODYNAMIQUE
TA1000/1000C
Tunnel Aérodynamique, 1000X1000 mm, Contrôlé par Ordinateur (PC)
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.- AÉRODYNAMIQUE
TA1200/1200C
Tunnel Aérodynamique, 1200X1200 mm, Contrôlé par Ordinateur (PC)
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.- AÉRODYNAMIQUE
TACL2000/2000C
Tunnel Aérodynamique Fermé, 2000X2000 mm, Contrôlé par Ordinateur (PC)
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.- VISUALISATION DE FLUX
TAVF180/100
Tunnel Aérodynamique pour la Visualisation de l'écoulement
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.- AÉRODYNAMIQUE
TADV225/450
Tunnel de Démonstration de Vol Aérodynamique
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.- AÉRODYNAMIQUE
ATBB
Banc d'Essais Aérodynamiques
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...