Vertical take of and landing aircraft with fluidic propulsion system

An aircraft, comprising:

• a fuselage;
• at least one primary airfoil having a first upper surface, the first upper surface having at least one recess disposed therein;
• at least one conduit in fluid communication with the at least one recess;
• at least one ejector disposed within the at least one recess, the at least one ejector configured to receive compressed air via the at least one conduit, the at least one ejector configured to produce a propulsive efflux stream;
• and
• at least one secondary airfoil coupled to the at least one primary airfoil and having a second upper surface, the at least one ejector being positioned such that the efflux stream flows over the second surface, the second surface being oriented so as to entrain the efflux stream to flow in a direction substantially perpendicular to the first upper surface.