Major experimental facilities

Evaluation System of Solid Oxide Fuel Cell

Wind Tunnel for Evaluation of Turbulence Feedback Control

Cross section : 50 mm x 500 mm
Total length: 7000 mm
Flow speed: 3 - 15 m/s

Jet Combustion Control Experimental Facility

nozzle diameter 20mm; cross section, 60x60mm; height, ca. 2m

Micro Gas Turbine Cogeneration Test Facility

Capstone Turbine Corp., 28kW

Measurement system

3-dimensional Particle Image Velocimetry（3-D PIV)

• CCD Camera x 2 (La Vision, Flow Master)
• Nd:YAG Pulse Laser (Thales Laser Inc., dual 400mJ @ 10 Hz)
• Nd:YAG Pulse Laser (NewWave Research Inc., 25mJ @ 60 Hz)

Laser Induced Fluorescence（LIF）　　

• ICCD Camera (La Vision, FlameStar2)
• Nd:YAG laser (Lamda Physik)
• Dye laser (Lamda Physik, ScanMate)

Laser Doppler Velocimetry（LDV）　　

• 2-D fiber probe (DANTEC, 60X11)
• BSA x 2
• 4W Ar laser

Hot wire/film anemometer

• CTA

Computer system in THT lab.

File servers

Plat' Home, 4 TB HDD

JCS, Vintage, 2 TB HDD

INTEL Celeron1.1A GHz x 1, TR-SDRAM 256MB, 960GB HD

PC Cluster (Pentium4 2.0GHz, 2GB, 100GB) x 8 + HDD (SCSI, Raid 5) 720GB + HDD (SCSI, Raid 0) 720GB

Feedback Control System for Wall Turbulence

• DSP5111 (PPC7410, 500 MHz, 512 MB) x 2
• 14 bit, 196 ch AD
• 14 bit, 96 ch DA

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Last update: 2007-10-23.