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  2. Nozzle - Wikipedia

    en.wikipedia.org/wiki/Nozzle

    A nozzle is a device designed to control the direction or characteristics of a fluid flow (specially to increase velocity) as it exits (or enters) an enclosed chamber or pipe. A nozzle is often a pipe or tube of varying cross sectional area, and it can be used to direct or modify the flow of a fluid ( liquid or gas ).

  3. Spray nozzle - Wikipedia

    en.wikipedia.org/wiki/Spray_nozzle

    A spray nozzle or atomizer is a device that facilitates the dispersion of a liquid by the formation of a spray. The production of a spray requires the fragmentation ...

  4. de Laval nozzle - Wikipedia

    en.wikipedia.org/wiki/De_Laval_nozzle

    A de Laval nozzle (or convergent-divergent nozzle, CD nozzle or con-di nozzle) is a tube which is pinched in the middle, with a rapid convergence and gradual divergence. It is used to accelerate a compressible fluid to supersonic speeds in the axial (thrust) direction, by converting the thermal energy of the flow into kinetic energy .

  5. Plug nozzle - Wikipedia

    en.wikipedia.org/wiki/Plug_nozzle

    Sectioned Jumo 004 exhaust nozzle, showing the Zwiebel restrictive body. The jet-engine plug nozzle has its origins in rocketry [2] but has also been studied over the years, but not used, for supersonic cruise aircraft such as the Boeing SST, [3] the proposed General Electric Variable Cycle Engine, with its acoustic plug nozzle, [4] and Concorde.

  6. Propelling nozzle - Wikipedia

    en.wikipedia.org/wiki/Propelling_nozzle

    A propelling nozzle is a nozzle that converts the internal energy of a working gas into propulsive force; it is the nozzle, which forms a jet, ...

  7. Rocket engine nozzle - Wikipedia

    en.wikipedia.org/wiki/Rocket_engine_nozzle

    Figure 1: A de Laval nozzle, showing approximate flow velocity increasing from green to red in the direction of flow Density flow in a nozzle. A rocket engine nozzle is a propelling nozzle (usually of the de Laval type) used in a rocket engine to expand and accelerate combustion products to high supersonic velocities.

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