J-GLOBAL ID:201110079242889025   Research Resource code:1000000686 Update date:Dec. 13, 2002

Arbitrarily inclineable low speed wind tunnel.

Owning Organization:
Contact: NAKAMURA Yoshiaki
Resource classification: Experience equipment, Facilities, etc
Research area  (1): Aerospace engineering
Arbitrarily inclineable low speed wind tunnel:
The purpose is to measure the aerodynamic
characteristics of model airplanes.
User environment and conditions:
Must not obstruct research activities.
User procedures and method:
Need approval of the Committee of Wind Tunnel, Aviation
Department (regulations).

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