The effect of large deformation in the flow between the bellmouth and centerbody is considered analytically for application to studies of vortex breakdown in a pipe. Basic equations are defined for axisymmetric inviscid swirling flows at the inflow and outflow sections. Axial and circumferential velocity component profiles are presented, and comparisons are made with trials involving vane angles of 42 deg and Re of 2300. Axial components of the prediction matched well in the inner half of the pipe radius and not well with the outer, while circumferential predictions were good only at the axis. A lack of viscosity was concluded to result in the inaccuracies near the wall.
Axisymmetric inviscid swirling flows produced by bellmouth and centerbody
AIAA Journal ; 20
1982-04-01
Miscellaneous
No indication
English
Inviscid Swirling Flows through a Choked Nozzle
AIAA | 1973
|SAE Technical Papers | 1980