MULTI-DIMENSIONAL FLOW ANALYSIS OF GOLDBERG FALCON REMOTE CONTROLLED AIRCRAFT WING

The wing is very important part of the airplane assists in producing the lift required for the flight. This work simulates the flow over a three-dimensional design of the falcon wing and tries to analyze the streamline pattern over the wing. This particular design of the wing is used in Carl Goldberg Falcon 56 Mk II R/C power plane. Flow properties around the wing as well on the wing surface body have been analyzed by using K-epsilon turbulence model. Flow patterns over the cross-section of the wing were analyzed and clearly plotted by using different contours of pressure temperatures and velocities.