No. 105, 1999, 33-45
Numerical approach to study the non-stationary flow phenomena in exhaust hood compartment - last stage of steam turbine
VALERY G. SOLODOV
Abstract
The paper describes 3D numerical models and some results of numerical simulation of self-excited oscillatory flow regimes through exhaust difiusers of large steam turbines operating jointly with last stage.
Keywords:
axisymmetrical flow, circular diffuser, shock wave movementDownload: