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Journal Articles
Accepted Manuscript
Article Type: Research-Article
J. Eng. Gas Turbines Power.
Paper No: GTP-22-1037
Published Online: August 11, 2022
Journal Articles
Accepted Manuscript
Article Type: Research-Article
J. Eng. Gas Turbines Power.
Paper No: GTP-22-1246
Published Online: August 11, 2022
Journal Articles
Accepted Manuscript
Article Type: Research-Article
J. Eng. Gas Turbines Power.
Paper No: GTP-22-1004
Published Online: August 9, 2022
Journal Articles
Accepted Manuscript
Article Type: Research-Article
J. Eng. Gas Turbines Power.
Paper No: GTP-22-1240
Published Online: August 9, 2022
Journal Articles
Accepted Manuscript
Article Type: Research-Article
J. Eng. Gas Turbines Power.
Paper No: GTP-22-1270
Published Online: August 9, 2022
Journal Articles
Accepted Manuscript
Article Type: Research-Article
J. Eng. Gas Turbines Power.
Paper No: GTP-22-1377
Published Online: August 9, 2022
Journal Articles
Accepted Manuscript
Article Type: Research-Article
J. Eng. Gas Turbines Power.
Paper No: GTP-22-1056
Published Online: August 9, 2022
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. September 2022, 144(9): 091007.
Paper No: GTP-22-1223
Published Online: August 1, 2022
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. September 2022, 144(9): 091006.
Paper No: GTP-22-1116
Published Online: August 1, 2022
Image
in Identification of Mistuning Based on Forced Response Measurements and Assessment for a Real Compressor Blisk
> Journal of Engineering for Gas Turbines and Power
Published Online: August 1, 2022
Fig. 1 Schematic illustration of substructuring approach More
Image
in Identification of Mistuning Based on Forced Response Measurements and Assessment for a Real Compressor Blisk
> Journal of Engineering for Gas Turbines and Power
Published Online: August 1, 2022
Fig. 2 Finite element model of academic blisk's initial sector with blade (light gray), disk sector (dark gray), and simulated measured degree-of-freedom (red dot). The disk sector contains 836 and the blade 1250 C3D20 elements leading to a total of 33,432 nodal degrees-of-freedom. More
Image
in Identification of Mistuning Based on Forced Response Measurements and Assessment for a Real Compressor Blisk
> Journal of Engineering for Gas Turbines and Power
Published Online: August 1, 2022
Fig. 3 (Top) Dispersion diagram of the academic blisk; (bottom) zoom 1F mode family More
Image
in Identification of Mistuning Based on Forced Response Measurements and Assessment for a Real Compressor Blisk
> Journal of Engineering for Gas Turbines and Power
Published Online: August 1, 2022
Fig. 4 Frequency response data of 2EO resonance crossing used as identification input, with tuned response (black dotted line) for comparison More
Image
in Identification of Mistuning Based on Forced Response Measurements and Assessment for a Real Compressor Blisk
> Journal of Engineering for Gas Turbines and Power
Published Online: August 1, 2022
Fig. 5 (Top) Identified mistuning factors for 1F mode family; (bottom) relative errors More
Image
in Identification of Mistuning Based on Forced Response Measurements and Assessment for a Real Compressor Blisk
> Journal of Engineering for Gas Turbines and Power
Published Online: August 1, 2022
Fig. 6 Measured DOFs on the industrial blisk (red dots) More
Image
in Identification of Mistuning Based on Forced Response Measurements and Assessment for a Real Compressor Blisk
> Journal of Engineering for Gas Turbines and Power
Published Online: August 1, 2022
Fig. 7 (Top) Dispersion diagram of the industrial blisk; (middle) zoom 3T mode; (bottom) zoom 1C mode More
Image
in Identification of Mistuning Based on Forced Response Measurements and Assessment for a Real Compressor Blisk
> Journal of Engineering for Gas Turbines and Power
Published Online: August 1, 2022
Fig. 8 Input frequency responses of DOF 1 for resonance crossing of 3T mode family with 2EO More
Image
in Identification of Mistuning Based on Forced Response Measurements and Assessment for a Real Compressor Blisk
> Journal of Engineering for Gas Turbines and Power
Published Online: August 1, 2022
Fig. 9 Identified mistuning factors for 3T mode family, using response of 5 DOFs on each blade, 1 DOF on each blade, and 1 DOF on only 20 of the 26 blades More
Image
in Identification of Mistuning Based on Forced Response Measurements and Assessment for a Real Compressor Blisk
> Journal of Engineering for Gas Turbines and Power
Published Online: August 1, 2022
Fig. 10 Reconstructed frequency response versus input for resonance crossing of 3T mode family with 2EO: best residual DOF 1 More
Image
in Identification of Mistuning Based on Forced Response Measurements and Assessment for a Real Compressor Blisk
> Journal of Engineering for Gas Turbines and Power
Published Online: August 1, 2022
Fig. 11 Reconstructed frequency response versus input for resonance crossing of 3T mode family with 2EO: worst residual DOF 1 More