Vortex breakdown in a hydro turbine draft tube swirling jet
Artur Gesla, Eunok Yim
TL;DR
This work analyzes vortex rope formation in a Francis turbine draft-tube by treating the rope as a vortex-breakdown instability of a swirl-dominated, axisymmetric baseflow in a laminar setting. Using linear stability analysis and direct numerical simulations on a simplified diffuser–pipe domain, it identifies a supercritical Hopf bifurcation of the $m=1$ mode at $Re_c \approx 2340.86$ with dominant frequency $ω \approx 1.262$, leading to a saturated monohelical vortex rope whose amplitude scales as $\sqrt{Re-Re_c}$. Boundary conditions markedly alter the bifurcation: no-slip walls give the classical Hopf scenario, while free-slip walls yield axis-centered recirculation, two saddle-node folds and a breathing, hysteretic dynamics, with an imperfect transcritical unfolding observed as inflow swirl (BEP) changes. The results illuminate how vortex rope-like structures emerge from vortex breakdown in turbine geometries and point to future work incorporating turbulence models to bridge toward realistic turbulent rope dynamics.
Abstract
The swirling flow in a Francis type hydropower turbine is known to be susceptible to the formation of a large helical structure, commonly referred to as a vortex rope. This vortex rope can be interpreted as an unstable mode associated with vortex breakdown. This perspective is adopted here in a simplified laminar flow setting. The helical vortex rope mode is shown to bifurcate supercritically from an axisymmetric baseflow in a Hopf bifurcation within a turbine draft tube. When wall friction effects are neglected, a large recirculation region at the axis can form and a range of subcritical solutions is identified for a flow regime corresponding to partial load of the turbine. The existence of these subcritical solutions promotes the emergence of a hysteresis loop. We further describe a regular dynamics of a formation of recirculation bubble at the axis and its destruction due to the emergence of a helical vortex rope at its periphery. Increasing the axial flow discharge towards the regime corresponding to nominal turbine load leads to an unfolding of the steady solutions branch in a transcritical bifurcation. This bifurcation takes place at finite Reynolds number and complements existing evidence of transcritical bifurcation of the swirling jet flows, previously reported only in the inviscid limit.
