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Showing 1 to 3 of 3 for “"Convergent Nozzle"”.

  1. A Study of an Asymmetric Two-Dimensional Nozzle as A Vector-Thrust Device

    … flow through an asymmetric two-dimensional convergent nozzle is solved by employing the method of hodograph transformation, coupled with finite-difference computation. With the given appropriate flow parameters, solution of the flow problem is first established in the hodograph domain. The …

    uiuc Repository record for A Study of an Asymmetric Two-Dimensional Nozzle as A Vector-Thrust Device (opens in a new tab)

  2. CFD simulation of flow fields associated with high speed jet impingement on deflectors

    … turbulent free jets produced by a simple convergent nozzle were analyzed. These include a subsonic jet with p₁/pâ =1 and M₁=0.57, a moderately under-expanded jet with p₁/pâ =1.42 and M₁=1, and a highly under-expanded jet with p₁/pâ =3.57 and M₁=1. The reflecting shocks associated with the …

    vt Repository record for CFD simulation of flow fields associated with high speed jet impingement on deflectors (opens in a new tab)

  3. Advancing Exhaust Flow Uniformity, Operational Stability, and Total Pressure Gain of Rotating Detonation Engines for Successful Turbine Integration

    … Firstly, RDC exit was configured with a convergent nozzle (CN) of varying RDC throat area ratio (ARC = 1.0 to 2.0) to increase the chamber pressure and total pressure gain (TPG). The 100 kHz particle image velocimetry (PIV) at RDC exit showed reductions in flow unsteadiness with …

    alabama Repository record for Advancing Exhaust Flow Uniformity, Operational Stability, and Total Pressure Gain of Rotating Detonation Engines for Successful Turbine Integration (opens in a new tab)