TAS25/100C Computer Controlled Supersonic Wind Tunnel

8.6.- AERODINAMIKA
COMPUTER CONTROLLED SUPERSONIC WIND TUNNEL - TAS25/100C

SISTEM INOVATIF

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.

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FSS

Sistem Simulasi Kegagalan
PLCHMI

Kontrol dan Pemantauan IIoT Lokal/Jarak Jauh dengan HMI
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GAMBARAN UMUM

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.

LATIHAN DAN PRAKTEK PEDOMAN

LATIHAN PRAKTIS YANG DIANDAL TERMASUK DALAM PANDUAN

  1. Pressure distribution in subsonic and supersonic flows.
  2. Calculation of the air velocity inside a supersonic wind tunnel.
  3. Comparison between experimental and theoretical pressure profile.
  4. Pressure distribution in a two-dimensional model under subsonic and supersonic flows.
  5. Influence of the attack angle on the forces exerted on a double wedge model.
  6. Shock wave display (required TAS25/100-SO accessory).
  7. Determination of Mach number from the shock wave angle (required TAS25/100-SO accessory).
  8. Experimental testing of the relationship between corner angle, Mach number and shock wave angle (required TAS25/100-SO accessory).

LEBIH BANYAK LATIHAN PRAKTIS YANG AKAN DILAKUKAN DENGAN UNIT

  1. Many students view results simultaneously. To view all results in real time in the classroom by means of a projector or an electronic whiteboard.
  2. 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.
  3. The Computer Control System with SCADA allows a real industrial simulation.
  4. This unit is totally safe as uses mechanical, electrical/electronic, and software safety devices.
  5. This unit can be used for doing applied research.
  6. This unit can be used for giving training courses to Industries even to other Technical Education Institutions.
  7. Control of the TAS25/100C unit process through the control interface box without the computer.
  8. Visualization of all the sensors values used in the TAS25/100C unit process.
  9. Several other exercises can be done and designed by the user.

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