Publications by Carlos Tavera Guerrero
Peer reviewed
Conference papers
[1]
C. Tavera Guerrero et al., "Numerical surface roughness influence on the aerodamping of an axial transonic compressor at nominal speed and part-speed," in Proceedings of ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition, GT 2024, 2024.
[2]
N. Glodic, C. Tavera Guerrero and M. Gutierrez, "Aeroelastic Response of a Transonic Compressor Cascade at High Reduced Fequencies," in Proceedings of ISUAAAT16, 2022.
[3]
N. Glodic, C. Tavera Guerrero and M. Gutierrez, "Blade oscillation mechanism for aerodynamic damping measurements at high reduced frequencies," in E3S Web Conf.Volume 345, 2022XXV Biennial Symposium on Measuring Techniques in Turbomachinery (MTT 2020), 2022.
[4]
N. Glodic et al., "Bringing turbomachinery aeromechanics research closer to education," in ISUAAAT16, 2022.
[5]
C. Tavera Guerrero, N. Glodic and H. Mårtensson, "STEADY-STATE AERODYNAMICS TIP GAP INFLUENCE IN A TRANSONIC LINEAR CASCADE AT NEAR STALL," in 33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022, 2022, pp. 2131-2140.
[6]
C. Tavera Guerrero, N. Glodic and M. Hans, "Steady-state aerodynamics tip gap influence in atransonic linear cascade at near stall," in 33rd Congress of the International Council of the Aeronautical Sciences (ICAS), Stockholm, 4–9 September 2022, 2022.
[7]
C. Tavera Guerrero, N. Glodic and P. Groth, "Validation of Steady-State Aerodynamics in a Transonic Linear Cascade at Near Stall Conditions," in Proceedings of the ASME Turbo Expo, 2022.
[8]
C. Tavera Guerrero et al., "Validation of unsteady aerodynamics in a transonic linear cascade at first flex modeshape at near stall conditions," in ISUAAAT 16, 2022.
Non-peer reviewed
Other
[9]
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2024-11-21 00:34:00