International Journal of Gas Turbine, Propulsion and Power Systems
Online ISSN : 1882-5079
Volume 13, Issue 3
Displaying 1-2 of 2 articles from this issue
  • 2022 Volume 13 Issue 3 Pages 1-6
    Published: November 09, 2022
    Released on J-STAGE: November 11, 2022
    JOURNAL OPEN ACCESS
    Water droplet impingement on a low-pressure steam turbine blade causing erosion has been recognized as a crucial issue. It is essential to elucidate a comprehensive droplet detachment mechanism, not only from the trailing edge but also from the liquid film surface. In the present paper, we investigate the influence of interfacial friction factor against liquid film dynamics on a wall sheared by a turbulent gas flow, including the liquid film thickness, liquid film velocity and entrained droplet detached from liquid surface for both pipe flow and plate flow conditions. We conduct the analyses by using a liquid film dynamics model, recently established, considering the three-dimensional destabilized waves and droplet entrainment from the liquid surface. As a result, the film thickness and velocity greatly depends on the interfacial friction factor. Interestingly, the rate of entrained droplet to initial liquid film has a minimum value when the interfacial friction factor equals to the inverse of the liquid film Reynolds number, while the remaining liquid film flow rate becomes maximum.
    Download PDF (2232K)
  • 2022 Volume 13 Issue 3 Pages 7-13
    Published: November 09, 2022
    Released on J-STAGE: November 11, 2022
    JOURNAL OPEN ACCESS
    Thermal cycling tests are carried out under a temperature gradient using specimens of thermal barrier coating (TBC). Vertical cracks in the topcoat grow in the direction of the coating thickness, and transverse cracks in the topcoat, which can lead to delamination, grow in the vicinity of the interface with the bondcoat. At a temperature of 1223 K at the substrate surface, with a heat flux of 1.39 MW/m2, remarkable growth of transverse cracks is observed, whereas the growth is slower at lower temperatures and heat flux conditions. The transverse crack growth is evaluated using the energy release rate based on Hutchinson’s method. Further, the energy release rate is calculated for a TBC on an in-service blade of an F-class gas turbine. For this, the results from a numerical simulation for the temperature distribution of the blade are used. The criteria for crack growth that can lead to TBC delamination are discussed.
    Download PDF (1983K)
feedback
Top