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Wind tunnel / Soft matter / Sting / Aeronautical and Astronautical Research Laboratory / Pusher configuration / Fluid dynamics / Aerodynamics / Aerospace engineering
Date: 2013-10-01 11:13:30
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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