Supply Result
| Year | Customer | Equipment | Remarks (specifications) |
|---|---|---|---|
| 1960 | For the laboratory | 2-m Transonic Wind Tunnel | Type : Adjustable pressure, single feed-back closed type Test : section 2×2m Max. Mach number : 1.4 Blower : 22,500kW |
| 1965 | For the laboratory | Trisonic Wind Tunnel | Type : Blow-down type Test section : 450×450mm Mach number : 0.6 to 4.2 Nozzle : Flexible nozzle |
| 1966 | For the university | Hyper-Speed Aerodynamic Experimental Facility | Type : Blow-down type (1) Supersonic wind tunnel Test section : 150×150mm Mach number : 2 to 5 Stagnation temperature : 600°C Duration time : 5 minutes (2) Transonic wind tunnel Test section : 450×250mm Mach number : 0.4 to 1.2 |
|
1968 |
For our company | Trisonic Wind Tunnel | Type : Blow-down type Test section : 600×600mm Mach number : 0.4 to 4 Nozzle : Flexible nozzle |
| 1972 | For the university | Adjustable -Density Transonic Fluidization Facility | Test Section : 200×300×750mm Mach number : 0.3 to 1.0 Compressor : 4-stage axial flow type with fixed-pitch rotor blades Motor : 3-phase, 300-kW wound-rotor induction motor Pressure in shell : 0.02 to 0.1 MPa |
| 1989 | For the laboratory | ISAS Supersonic and Transonic Wind Tunnels | [Transonic wind tunnel] Type : Downwash type Test section : 600×600mm Range of Mach number : 0.3 to 1.3 (adjustable) Measuring time : 30 seconds or more [Hypersonic wind tunnel] Type : Downwash type Test Section : 600×600mm Range of Mach number : 1.5 to 4.0 (adjustable) Measuring time : 30 seconds or more |
