Computer Controlled Supersonic Wind Tunnel

อุโมงค์ลมความเร็วเหนือเสียงที่ควบคุมด้วยคอมพิวเตอร์ เป็นอุโมงค์ลมแบบเปิดสำหรับการศึกษาคุณสมบัติแอโรไดนามิกของวัตถุลากต่างๆ ที่ขึ้นอยู่กับการไหลของกระแสใต้เสียงและความเร็วเหนือเสียง

EXERCISES AND PRACTICAL POSSIBILITIES TO BE DONE WITH THE MAIN ITEMS

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).
   Other possibilities to be done with this Unit:
9. Many students view results simultaneously.
   To view all results in real time in the classroom by means of a projector or an electronic whiteboard.
10. 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.ises can be done and designed by the user
11. The Computer Control System with SCADA allows a realindustrial simulation.
12. This unit is totally safe as uses mechanical, electrical/electronic, and software safety devices.
13. This unit can be used for doing applied research.
14. This unit can be used for giving training courses to Industries even to other Technical Education Institutions.
15. Control of the TAS25/100C unit process through the control interface box without the computer.
16. Visualization of all the sensors values used in the TAS25/100C
    unit process.
    – Several other exercises can be done and designed by the user