2020
DOI: 10.1080/10407782.2020.1713692
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Numerical investigation of particle deposition in film-cooled blade leading edge

Abstract: This study numerically investigates film-cooling performance and particle trajectories in AGTB (two rows of cylindrical holes equipped on suction side (SS) and pressure side (PS) of the leading edge, respectively) turbine cascade. Particle deposition on a turbine blade is analyzed by calculations of capture efficiency and impact efficiency. The turbulent flow is modeled by the Realizable k-e turbulence model, and the discrete phase model (DPM) with user-defined functions (UDFs) is used to simulate the particle… Show more

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Cited by 11 publications
(4 citation statements)
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“…The convergence criterion is that the residual of each governing equation is less than 1.0 × 10 −4 except that the energy equation is 1.0 × 10 −6 . It is assumed that the interaction or impact between particles and the influence of particle phase on fluid phase are ignored, which allows for an adoption of a one-way coupling for the particle phase [37]. A stochastic tracking model associated with discrete random walk is used to predict the turbulent dispersion of particles in the continuous phase, and the particles are monitored till they exit the computational domain.…”
Section: Methodsmentioning
confidence: 99%
“…The convergence criterion is that the residual of each governing equation is less than 1.0 × 10 −4 except that the energy equation is 1.0 × 10 −6 . It is assumed that the interaction or impact between particles and the influence of particle phase on fluid phase are ignored, which allows for an adoption of a one-way coupling for the particle phase [37]. A stochastic tracking model associated with discrete random walk is used to predict the turbulent dispersion of particles in the continuous phase, and the particles are monitored till they exit the computational domain.…”
Section: Methodsmentioning
confidence: 99%
“…The volume of the particle is less as compared to the air volume so the effect of particles on the turbulence of airflow and collusion between particles is neglected. 21,32 The particles to gas density ratios are very large therefore the force of the pressure gradient and virtual mass cannot be considered. The rotation and collision of the particles are ignored.…”
Section: Particle Motion Discrete Phase Modelingmentioning
confidence: 99%
“…17,18 The particle deposition rate was numerically investigated to examine the effect of different types of roughness elements and the results showed the significance of roughness elements for the particles deposition and deposition velocity. [19][20][21] The deposition rate of particles strongly depends on Reynolds number, shape of roughness element, and size of the duct. [22][23][24] Further to this, flow characteristics and turbulence intensity also affect the deposition process.…”
Section: Introductionmentioning
confidence: 99%
“…A computational analysis was performed by Bowen et al 13 to determine if particle impact events on the external surface of gas turbine engine blades can be faithfully replicated in an experimental rotor cascade, they found that the lack of a vane in the cascade causes drastically different particle inlet vectors over the rotor than those are seen in the engine and the particle size affects its impacting location. Wang et al 14 numerically studied the particle deposition on a turbine blade with diameters of 1–50 μm, and a parameter named invasion efficiency was proposed to analyze the invasion of particles into the film hole. It was found that smaller particles result in lower invasion efficiency, and larger particles are more likely to invade into the film-cooling hole especially at a low blowing ratio.…”
Section: Introductionmentioning
confidence: 99%