Rsrc
J-GLOBAL ID:201110062628373872   Research Resource code:5000002713 Update date:Nov. 01, 2004

1m×1m Supersonic Wind Tunnel

1m×1m 超音速風洞
Owning Organization:
Contact: HAMAMOTO Shigeru
Resource classification: Experience equipment, Facilities, etc
Overview:
Main Objectives: To study aerodynamics in supersonic
flight and to research and develop the supersonic
transport and supersonic projectile.
Performance: Test Section 1m×1m
Duration more than 40 seconds.
Mach Number 1.4~4.0 Compressor,
Air Compressor common use with the transonic wind tunnel.
Completion Year: FY 1961.
Use: To study aerodynamics in supersonic flight and to
research and develop the supersonic transport and
supersonic projectile.
User environment and conditions:
Instruments on models, sensor/data transfer are to be prepared by a user as a rule
User procedures and method:
Refer to Web Page of JAXA

Return to Previous Page