J-GLOBAL ID:201110091009076170   Research Resource code:5000003250 Update date:Nov. 01, 2004

0.2m×0.2m Supersonic Wind Tunnel

Owning Organization:
Contact: HAMAMOTO Shigeru
Resource classification: Experience equipment, Facilities, etc
Supersonic wind tunnel with 20 cm X 20 cm of measured
section. Mach number of 1.5 to 2.5.
Constructed in 1994, and renovation of contraction
wall in 1999
Type: Successive cyclic
Use: Aerodynamic research under hypersonic low
turbulence environment
User procedures and method:
Refer to Web Page of JAXA.

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