Supply Result
| Year | Customer | Equipment Name | Remarks (specifications) |
|---|---|---|---|
| 1960 | For the university | 15cm High-Speed Wind Tunnel | Type : Blow-down Type Test Section : 150×150mm Max. Mach Number : 4.5 |
| 1961 | For the laboratory | 40cm Supersonic Wind Tunnel | Type : Blow-down type Spherical Tank : φΦ 10m, 1.47 MPa Test Section :400×400mm Mach Number : 1.5 to 4 |
| 1963 | For our company | 25cm Supersonic Wind Tunnel | Type : Adjustable Pressure, Closed Circuit Test Section : 250×250mm Max. Mach Number : 4.0 Blower : 1,300kW |
| 1966 | For the university | Hyper-speed Aerodynamic Experimental Facility | Type : Blow-down type (i) Supersonic Wind Tunnel Test Section : 150×150mm Mach Number : 2 to 5 Stagnation Temperature : 600°C Duration Time : 5 minutes (ii) Transonic Wind Tunnel Test Section : 450×250mm Mach Numbe : r0.4 to 1.2 |
| 1968 | For our company | Supersonic Wind Tunnel | Type : Blow-down type Test Section : 600×600mm Mach Number : 0.4 to 4 Nozzle Type : Flexible Nozzle |
| 1989 | For the laboratory | ISAS Supersonic and Transonic Wind Tunnels | [Transonic Wind Tunnel] Type : Downwash Type Test Section : 600×600mm Mach number : 0.3 to 1.3 (adjustable) Measuring Time : 30 seconds or more [Supersonic Wind Tunnel] Type : Downwash Type Test Section : 600×600mm Mach Number Range : 1.5 to 4.0 (adjustable) Measuring Time : 30 seconds or more |
| 1994 | For the university | Supersonic Wind Tunnel | Type : Blow-off type Blow Port Size : 80mm×40mm Mach Number : 1.5 |
| 1999 | For the university | Supersonic Measurement Analysis and System | Type : Blow-out with vacuum suction type Mach Number : 2 and 4 Test Section : 80×80mm×1500mm (closed type) 80×80mm×80mm (free jet type) Measuring Time : 10 seconds or more (one blow each 30 minutes available) |
