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Wind tunnel / Soft matter / Sting / Aeronautical and Astronautical Research Laboratory / Pusher configuration / Fluid dynamics / Aerodynamics / Aerospace engineering


Adapting to Limitations of a Wind Tunnel Test Facility in the Aerodynamic Testing of a new UAV Dr K.C. Wong, Mr H.J.H. Peters1, Mr P. Catarzi2 School of Aerospace, Mechanical and Mechatronic Engineering University of Syd
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Document Date: 2013-10-01 11:13:30


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File Size: 1,31 MB

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City

Hogeschool Haarlem / /

Company

Brumby Mk II incorporated / X5 / /

Country

United States / Netherlands / Italy / /

Currency

CAD / /

Facility

Wind Tunnel / Low Speed Wind Tunnel / University of Sydney / Mechatronic Engineering University of Sydney NSW / The University of Sydney / University of Ohio / /

IndustryTerm

room to accommodate additional equipment / wind tunnel equipment / aerodynamic devices / /

Organization

Politecnico di Torino / School of Aerospace / Aerospace / Mechanical and Mechatronic Engineering University of Sydney NSW / University of Ohio / Wind Tunnel Lab. / P. Catarzi2 School of Aerospace / Aeronautical Engineering Department / Australian Centre for Field Robotics / University of Sydney / Department of Aeronautical Engineering / /

Person

Min Speed / K.C. Wong / Ty / /

Position

Tz Nm Transducer model / servo motor controller / /

Product

Torino / delta wing / /

ProvinceOrState

Ohio / /

Technology

CAD / /

SocialTag