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NARROW
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1-20 of 55210
Keywords: ORC turbine
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Journal Articles
Accepted Manuscript
Journal:
Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach.
Paper No: TURBO-24-1377
Published Online: March 20, 2025
Journal Articles
Journal:
Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2025, 147(10): 101007.
Paper No: TURBO-24-1291
Published Online: March 20, 2025
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 1 Illustrations of Geometry 1–4 used in the simulations in this paper More about this image found in Illustrations of Geometry 1–4 used in the simulations in this paper
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 2 Midspan-section illustrations of Geometry 1–4 with geometric minimum area lines highlighted More about this image found in Midspan-section illustrations of Geometry 1–4 with geometric minimum area l...
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 3 Schematic of ECAT facility working section (without combustor simulator), adapted from [ 11 ] More about this image found in Schematic of ECAT facility working section (without combustor simulator), a...
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 4 Computational domain (Geometry 1) for simulations More about this image found in Computational domain (Geometry 1) for simulations
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 5 Midspan view of the mesh (Geometry 1) More about this image found in Midspan view of the mesh (Geometry 1)
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 6 Distributions of normalised local KE loss coefficient, ζ ′ / ζ ref ″ ″ , for Geometry 1–4 for experiment and CFD predictions. Data are viewed from downstream (VFD); the principal exit flow direction is CW VFD More about this image found in Distributions of normalised local KE loss coefficient, ζ ′ / ζ ...
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 7 CFD-predicted axial vorticity distributions, ω x , for uncooled RANS and cooled RANS. Data are VFD; the exit flow direction clockwise VFD More about this image found in CFD-predicted axial vorticity distributions, ω x , for uncooled RAN...
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 8 Axial vorticity distributions, ω x , from CFD prediction for Geometry 1–4. Data are VFD; the exit flow direction CW VFD More about this image found in Axial vorticity distributions, ω x , from CFD prediction for Geomet...
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 9 Schematic representation of burn-back vortices for Geometry 4, visualised by Q-criterion More about this image found in Schematic representation of burn-back vortices for Geometry 4, visualised b...
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 10 Radial distributions of circumferentially mass-flux-averaged kinetic energy loss coefficient, ζ ″ ( r ) , for Geometry 1–4 for experiment and CFD predictions More about this image found in Radial distributions of circumferentially mass-flux-averaged kinetic energy...
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 11 CFD-predicted vane surface streamlines for Geometry 1 and Geometry 4 on the SS and PS More about this image found in CFD-predicted vane surface streamlines for Geometry 1 and Geometry 4 on the...
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 12 Radial distributions of circumferentially mass-flux-averaged exit flow angle, β ′ ( r ) , for Geometry 1–4 for experiment and CFD predictions More about this image found in Radial distributions of circumferentially mass-flux-averaged exit flow angl...
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 13 Maximum flow angle deviation (from nominal) with burn-back damage depth More about this image found in Maximum flow angle deviation (from nominal) with burn-back damage depth
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 14 CFD-predicted NGV surface isentropic Mach number distributions at 15%, 50%, and 85% span for Geometry 1–4 More about this image found in CFD-predicted NGV surface isentropic Mach number distributions at 15%, 50%,...
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 15 CFD-predicted normalised PS and SS BL profiles for Geometry 1–4 at five different span locations More about this image found in CFD-predicted normalised PS and SS BL profiles for Geometry 1–4 at five dif...
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 16 CFD-predicted normalised PS and SS displacement thicknesses for Geometry 1–4 at five different span locations More about this image found in CFD-predicted normalised PS and SS displacement thicknesses for Geometry 1–...
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 17 CFD-predicted spanwise distribution of normalised boundary layer KE dissipation coefficient, e KE , for Geometry 1–4 More about this image found in CFD-predicted spanwise distribution of normalised boundary layer KE dissipa...
Image
in Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance
> Journal of Turbomachinery
Published Online: March 20, 2025
Fig. 18 CFD-predicted BL loss coefficients for Geometry 1–4 More about this image found in CFD-predicted BL loss coefficients for Geometry 1–4
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