6.5mx5.5m low speed wind tunnel
Utilization including for the acquisition of aerodynamic characteristics when taking off or landing an aircraft or when in low speed flight
| Department | Department Aviation Technology Directorate |
|---|---|
| Specifications | Type: Continuous circulation type Test section measurements: Height: 6.5 m, width: 5.5 m, 1 m cut off the four corners to create an octagonal cross section Wind speed: Maximum: 70 m/s, minimum: 1 m/s Blower: Combined use of variable pitch angle method and rotating speed control method: 3,000 kW Test cart: Strut cart (pyramid-type 6-component balance) Sting cart (internal balance) (4 degrees of freedom) Ground effect testing device: Moving belt system: 50 m/s max |
| Year of completion | FY 1965 FY 1994 (renew electric motor drive system, repair contraction cone, and increase test carts) |
| Usage fee | 326,928 yen/day (Current as of April 1, 2024) *The usage fee above includes the general management fee. *The usage fee above does not include technical fees, consumption tax and operational fees before and after testing. These fees will be charged separately. *The usage fee is calculated each fiscal year. In addition, prices may be revised without notice midway through the fiscal year. Inquire using the form below for details. |