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Journal Articles
Accepted Manuscript
Journal:
Journal of Turbomachinery
Article Type: Research Papers
J. Turbomach.
Paper No: TURBO-22-1259
Published Online: March 24, 2023
Journal Articles
Accepted Manuscript
Journal:
Journal of Turbomachinery
Article Type: Research Papers
J. Turbomach.
Paper No: TURBO-22-1050
Published Online: March 21, 2023
Journal Articles
Accepted Manuscript
Journal:
Journal of Turbomachinery
Article Type: Research Papers
J. Turbomach.
Paper No: TURBO-22-1366
Published Online: March 21, 2023
Journal Articles
Accepted Manuscript
Bryan Leicht, Brian Bohan, Fred Schauer, Ryan A. Kemnitz, Lisa Rueschhoff, Benjamin Lam, James W. Kemp, William Costakis
Journal:
Journal of Turbomachinery
Article Type: Research Papers
J. Turbomach.
Paper No: TURBO-22-1099
Published Online: March 13, 2023
Journal Articles
Accepted Manuscript
Dominik Ade, Johannes Eitenmueller, Sebastian Leichtfuss, Heinz-Peter Schiffer, Christoph Lyko, Gregor Schmid
Journal:
Journal of Turbomachinery
Article Type: Research Papers
J. Turbomach.
Paper No: TURBO-22-1224
Published Online: March 13, 2023
Journal Articles
Accepted Manuscript
David Fellows, Vincent Iskandar, Daniel Bodony, Ryan C. McGowan, Sang-Guk Kang, Aaron J. Pope, Chol-Bum M. Kweon
Journal:
Journal of Turbomachinery
Article Type: Research Papers
J. Turbomach.
Paper No: TURBO-22-1117
Published Online: March 8, 2023
Journal Articles
Accepted Manuscript
Journal:
Journal of Turbomachinery
Article Type: Research Papers
J. Turbomach.
Paper No: TURBO-22-1180
Published Online: March 8, 2023
Journal Articles
Journal:
Journal of Turbomachinery
Article Type: Research Papers
J. Turbomach. July 2023, 145(7): 071016.
Paper No: TURBO-21-1151
Published Online: March 6, 2023
Image
in Accounting for Circumferential Flow Nonuniformity in a Multistage Axial Compressor
> Journal of Turbomachinery
Published Online: March 6, 2023
Fig. 1 Reduced S1 vane count configuration of PAX101 More
Image
in Accounting for Circumferential Flow Nonuniformity in a Multistage Axial Compressor
> Journal of Turbomachinery
Published Online: March 6, 2023
Fig. 2 Compressor normalized total–total pressure map More
Image
in Accounting for Circumferential Flow Nonuniformity in a Multistage Axial Compressor
> Journal of Turbomachinery
Published Online: March 6, 2023
Fig. 3 Measurement locations for the traverses downstream of stator 1 and stator 2 More
Image
in Accounting for Circumferential Flow Nonuniformity in a Multistage Axial Compressor
> Journal of Turbomachinery
Published Online: March 6, 2023
Fig. 4 Normalized total pressure contours downstream of ( a ) stator 1 and ( b ) stator 2 from experiment More
Image
in Accounting for Circumferential Flow Nonuniformity in a Multistage Axial Compressor
> Journal of Turbomachinery
Published Online: March 6, 2023
Fig. 5 Effects of circumferential flow nonuniformity on stage efficiency characterization using single-passage pitchwise averaged profiles More
Image
in Accounting for Circumferential Flow Nonuniformity in a Multistage Axial Compressor
> Journal of Turbomachinery
Published Online: March 6, 2023
Fig. 6 Effects of circumferential flow nonuniformity on stage efficiency characterization using multipassage averaged profiles More
Image
in Accounting for Circumferential Flow Nonuniformity in a Multistage Axial Compressor
> Journal of Turbomachinery
Published Online: March 6, 2023
Fig. 7 Stator 1 downstream ( a ) passage–passage total pressure profile variability and ( b ) forcing function variability at 88% span More
Image
in Accounting for Circumferential Flow Nonuniformity in a Multistage Axial Compressor
> Journal of Turbomachinery
Published Online: March 6, 2023
Fig. 8 Stator 2 downstream ( a ) passage–passage total pressure profile variability and ( b ) forcing function variability at 88% span More
Image
in Accounting for Circumferential Flow Nonuniformity in a Multistage Axial Compressor
> Journal of Turbomachinery
Published Online: March 6, 2023
Fig. 9 Normalized total pressure measured at 50% span downstream of ( a ) stator 1 and ( b ) stator 2 More
Image
in Accounting for Circumferential Flow Nonuniformity in a Multistage Axial Compressor
> Journal of Turbomachinery
Published Online: March 6, 2023
Fig. 10 Comparison of spectral magnitudes calculated from discrete Fourier transform and multiwavelet approximation method for ( a ) stator 1 and ( b ) stator 2 profiles More
Image
in Accounting for Circumferential Flow Nonuniformity in a Multistage Axial Compressor
> Journal of Turbomachinery
Published Online: March 6, 2023
Fig. 11 Importance of the number of harmonics for reconstructing ( a ) stator 1 and ( b ) stator 2 total pressure field More
Image
in Accounting for Circumferential Flow Nonuniformity in a Multistage Axial Compressor
> Journal of Turbomachinery
Published Online: March 6, 2023
Fig. 12 Comparison of the reconstructed total pressure at midspan downstream of ( a ) stator 1 and ( b ) stator 2 with results from the experiment More
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