J-GLOBAL ID:201110076894316966   Research Resource code:5000002726 Update date:Dec. 15, 2003

0.6m×0.6m Transonic Flutter Testing Facility

0.6m×0.6m 遷音速フラッタ試験設備
Owning Organization:
Contact: TERADA Hiroyuki
Resource classification: Experience equipment, Facilities, etc
Main purpose: Experimental research on transonic flatter
Type: intermittent blow down wind tunnel
Dimension of test section: 60cm x 60cm
Mach number: 0.5 - 1.2
Designed total pressure: 147kPa - 392kPa (abs)
Mach number and total pressure can be swept.
User procedures and method:
[Procedure for Use]
Refer in detail to Business Squad, Planning Room.
[Charge for Use]
According to the calculation standard of acceptance
research expenses appointed by the Science and Technology
[Restriction for use]
Uses by a person not belonging to national administration
organs are limited to a case approved to be especially
necessary for improvement of aeronautical technology and
space technology.

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