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Experimental Studies on a Propelled Micro Air Vehicle
29th AIAA Applied Aerodynamics Conference
An experimental study has been carried out on a typical Micro Air Vehicle of span 300mm having inverse Zimmerman planform. The objective is to get i) the aerodynamic characteristics of the vehicle in the range of incidence and sideslip angle the vehicle expected to encounter during its flight; ii) an understanding of the propeller effect on the aerodynamic data and iii) the control surface (elevon) effectiveness with incidence. Tests were carried out in a low speed wind tunnel at a freestreamdoi:10.2514/6.2011-3656 fatcat:5jk4d24i4fctnjtpcmbx2cscl4