REPORT: WIND TUNNEL MEASUREMENT ON AN AEROPLANE MODEL
Report: Wind Tunnel Measurement On an Aero-plane Model
The experiment makes a great use of a wind tunnel to determine a few features of an aeroplane model. The results are used to determine the trimmed lift coefficient at the two tail settings with the CG assumed to be in a realistic position and the corresponding static margins and neutral points. The aircraft-less-tail has an aerodynamic centre position which was to be determined through calculations of the data achieved from the experiment. In finding out the lift curve slope of the aircraft, with or without the tail, a (1+ Continue reading...