Abstract: The present invention in one embodiment includes an aircraft having a fuselage with a powered propeller. The aircraft further includes a cambered main wing positioned aft of the fuselage and has a non cambered portion connected to the fuselage. The main wing also has a reflexed trailing edge and a non cambered ridge portion extending under the fuselage. A depression positioned in the non cambered portion of the main wing causes the fuselage to set in an airflow pattern of the propeller. The main wing includes both oversized fins extending upwardly from the ends of the main wing and sub-fins extending downwardly from the ends. The aircraft also includes V-shaped control wing positioned fore of the main wing and connected to a top portion of the fuselage by a mechanism for moving the control wing. In addition, the propeller is rotatably connected aft of the fuselage and above the main wing.