4   Artículos

 
en línea
Ken Wakimoto, Kazuhisa Chiba, Hiroyuki Kato and Kazuyuki Nakakita    
This study conducted wind tunnel tests with consecutive deflection angle changes on a three-dimensional (3D) wing with a control surface to procure aerodynamic data by sweeping the deflection angle. Configuration changes of a wind tunnel test model, such... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Kazuhisa Chiba, Tatsuro Komatsu, Hiroyuki Kato and Kazuyuki Nakakita    
We have developed a remote and precise feedback control system using optical measurement technology to alter the angle of a flap, which is part of a wind tunnel test model, automatically and to earn the aerodynamic data efficiently. To rectify the wastef... ver más
Revista: Aerospace    Formato: Electrónico

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