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Journal Articles
Journal:
Journal of Turbomachinery
Article Type: Research Papers
Publisher: ASME
J. Turbomach. November 2023, 145(11): 111004.
Paper No: TURBO-23-1147
Published Online: September 14, 2023
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 1 Illustration of TUDa-GLR-OpenStage test rig More about this image found in Illustration of TUDa-GLR-OpenStage test rig
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 2 Illustration of grid topology, flow domain, and boundary conditions of TUDa-GLR-OpenStage with a full-scale cavity seal More about this image found in Illustration of grid topology, flow domain, and boundary conditions of TUDa...
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 3 Validation of the full-scale model on predicting the overall performance of the TUDa-GLR-OpenStage with stator cavity More about this image found in Validation of the full-scale model on predicting the overall performance of...
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 4 Validation of the full-scale model on predicting the 2D distribution of the normalized difference in total pressure Δ π * at the design speed More about this image found in Validation of the full-scale model on predicting the 2D distribution of the...
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 5 Illustration of grid topology, flow domain, and boundary conditions of TUDa-GLR-OpenStage with a simplified cavity model More about this image found in Illustration of grid topology, flow domain, and boundary conditions of TUDa...
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 6 Contours of radial velocity, tangential velocity, and leakage swirl angle at a constant radius cut near plane D at the N100, NS condition More about this image found in Contours of radial velocity, tangential velocity, and leakage swirl angle a...
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 7 Validation of the simplified model on predicting the stage exit (ME30) radial profiles of flow angle and total pressure ratio at the design speed More about this image found in Validation of the simplified model on predicting the stage exit (ME30) radi...
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 8 Stage exit (ME30) 2D distribution of total pressure ratio at N100, NS condition More about this image found in Stage exit (ME30) 2D distribution of total pressure ratio at N100, NS condi...
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 9 Leakage flow ratio and leakage swirl angle under different incidences of the two operating speeds More about this image found in Leakage flow ratio and leakage swirl angle under different incidences of th...
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 10 Summary of overall compressor performance in variation with leakage flow ratio and leakage swirl angle at the design speed: ( a ) PE condition and ( b ) NS condition More about this image found in Summary of overall compressor performance in variation with leakage flow ra...
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 11 Isentropic efficiency penalty with different leakage flow ratios More about this image found in Isentropic efficiency penalty with different leakage flow ratios
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 12 Swirl-induced change in isentropic efficiency with different leakage flow ratios More about this image found in Swirl-induced change in isentropic efficiency with different leakage flow r...
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 13 Stator-inlet radial profiles of the incoming flow angle More about this image found in Stator-inlet radial profiles of the incoming flow angle
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 14 Stage exit (ME30) radial profiles of total pressure ratio using different leakage flow ratios More about this image found in Stage exit (ME30) radial profiles of total pressure ratio using different l...
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 15 Stage exit (ME30) 2D distribution: total pressure ratio of the nominal case (top row); normalized total pressure ratio difference between the α = 0 deg and m L / m =1.5% leakage case and the nominal case (bottom row) More about this image found in Stage exit (ME30) 2D distribution: total pressure ratio of the nominal case...
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 16 Limiting streamline and static pressure distribution on the hub and blade surfaces at the N100, NS condition (➀: hub corner separation; ➁: hub LE separation; ➂: near-hub TE separation; and ➃: near-shroud TE separation) More about this image found in Limiting streamline and static pressure distribution on the hub and blade s...
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 17 3D blockage volume in the stator passage at the N100, NS condition More about this image found in 3D blockage volume in the stator passage at the N100, NS condition
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 18 Stage exit (ME30) radial profiles of total pressure ratio using different leakage swirl angles under different operation conditions More about this image found in Stage exit (ME30) radial profiles of total pressure ratio using different l...
Image
in Characterizing Shrouded Stator Cavity Flow on the Performance of a Single-Stage Axial Transonic Compressor
> Journal of Turbomachinery
Published Online: September 14, 2023
Fig. 19 Stage exit (ME30) 2D distribution: total pressure ratio of the α = 0 deg leakage case (top row); normalized total pressure ratio difference between the α = + 40 deg and α = − 40 deg leakage cases (bottom row) More about this image found in Stage exit (ME30) 2D distribution: total pressure ratio of the α = 0 ...
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