Viscous swirling flow through transonic converging-diverging nozzles (with and without centerbodies) is examined numerically. An implicit technique is used to solve the axisymmetric Thin Layer Naiver-Stokes equations. The effect of swirl and viscosity on low Reynolds number flows is shown by examining integral parameters and flowfield details.
Analysis of a swirl stabilized arcjet thruster
1991-06-01
Conference paper
No indication
English
Analysis of a swirl stabilized arcjet thruster
AIAA | 1991
|Online Contents | 1996
|AIAA | 1996
|Medium power arcjet thruster experiments
AIAA | 1990
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