Method and nozzle for producing thrust

摘要: A method and apparatus for producing a thrust force from an annular axial stream of gaseous products fed to nozzle with supercritical pressure drop acceleration subsonic speed. In the nozzle, direction is changed radial divided into plurality opposing jets which collide in braking zone change back discharge ambient atmosphere. intensity (modulus) effected by changing flow rate and/or discharged Adjustment angle vector The comprises housing, central body flat base casing surrounding having end face profiled outlet edges forming together channel critical cross section outlet. axially adjustable angularly movable adjust position perpendicular longitudinal axis angular relative thereto.