Hypersonic wedge nozzle for chemical lasers
AssigneeThe United States of America as represented by the Secretary of the Army
InventorsDale L. Hook, John Waypa, Theodore A. Jacobs
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Abstract
A hypersonic wedge nozzle for chemical lasers that has a radially diverging low primary nozzle with a multiplicity of hypersonic wedge type secondary injection wedges at the exit end of the primary nozzle to allow gas flow to become supersonic in the primary nozzle before entering the regions between the secondary injection wedges or the surfaces thereof. Utilization of the large diverging primary nozzle in producing supersonic flow minimizes viscous effects in producing the supersonic flow in a chemical HF or DF laser.
Claims2
A hypersonic wedge nozzle for chemical lasers comprising a housing having a chamber therein and means for introducing a fluorine gas bearing stream into said chamber, a two-dimensional expansion nozzle leading from said chamber and having oppositely diverging walls, each of said walls having a width in the direction of flow through said two-dimensional expansion nozzle and a length which is perpendicular to said width, and a multiplicity of hypersonic secondary injection tubes mounted at the outlet defined by said walls and said tubes being positioned longitudinally of said walls, spaced from said walls and in the expanding area of said two-dimensional expansion nozzle, and said tubes having passages therein for injecting H.sub.2 or D.sub.2 for the chemical laser and being wedge-shaped from a front portion to a rear portion which contains said passages for injecting said H.sub.2 or D.sub.2, whereby an arrangement is provided for causing a resulting flow downstream of said tubes which retains greater velocity and total pressure when fluid flows through the arrangement and an arrangement in which the increase in static temperature brought about by viscous drag is restricted to a much smaller region of the flow field when fluid flows through said arrangement.
Dependencies are inferred from the claim text.