Abstract: A fluid injector consisting of an airfoil cross-sectioned rectangular plate mounted on and perpendicular to a pivoted hollow tube and suspended within a flowing stream of fluid into which another or the same type of fluid is to be injected through the tubular support exiting out the top surface of the plate and mixing with the primary fluid by means of vortices created at the rear side edges of the wing shaped plate. The quantity of injected fluid is controlled by the angle the plate is set in reference to the direction of flow of the primary fluid.