Publications by Nenad Glodic
Peer reviewed
Articles
[1]
S. Tian et al., "CFD-Aided Design of a Transonic Aeroelastic Compressor Rig," Journal of turbomachinery, vol. 141, no. 10, 2019.
Conference papers
[2]
A. Kaliyaperumal et al., "A numerical investigation of active flow control strategies for the suppression of aerodynamic flow separations in a very aggressive intermediate compressor duct," in Proceedings of ASME Turbo Expo 2024 : Turbomachinery technical conference and exposition, GT2024, vol 12c, 2024.
[3]
N. Glodic et al., "Aeroelastic tailoring of fan blades for an electric fan thruster," in ISABE 2024 @ Toulouse, FRANCE · 26th Conference of the International Society for Air Breathing Engines 22-27 Sep 2024, 2024.
[4]
K. Ananthakrishnan, N. Glodic and M. Gutierrez, "Influence of Circumferential Splitter Vane on Aerodynamics of Super Aggressive Intermediate Compressor Duct," in ISABE 2024, 2024.
[5]
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.
[6]
N. Glodic, C. Tavera Guerrero and M. Gutierrez, "Aeroelastic Response of a Transonic Compressor Cascade at High Reduced Fequencies," in Proceedings of ISUAAAT16, 2022.
[7]
A. P. Chalke, N. Glodic and M. Gutierrez, "Aeroelastic Tailoring of Compressor Blades," in ICAS PROCEEDINGS of 33th Congress of the International Council of the Aeronautical Sciences, Stockholm, Sweden, 2022.
[8]
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.
[9]
N. Glodic et al., "Bringing turbomachinery aeromechanics research closer to education," in ISUAAAT16, 2022.
[10]
T. Grönstedt et al., "MULTIDISCIPLINARY ASSESSMENT OF A YEAR 2035 TURBOFAN PROPULSION SYSTEM," in 33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022, 2022, pp. 4981-4990.
[11]
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.
[12]
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.
[13]
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.
[14]
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.
[15]
M. Lejon et al., "Multidisciplinary design of a three stage high speed booster," in Proceedings of the ASME Turbo Expo : Turbomachinery Technical Conference and Exposition, GT 2017, 2017.
[16]
N. Glodic, D. Vogt and T. Fransson, "Experimental and numerical investigation of mistuned aerodynamic influence coefficients in an oscillating LPT cascade," in Proceedings of the ASME Turbo Expo, 2012, pp. 1355-1367.
[17]
N. Glodic, D. Vogt and T. Fransson, "Influence of Tip Clearance Modelling in Predictions of Aeroelastic Response in an Oscillating LPT Cascade," in ISUAAAT 13; Tokyo, Japan, 11-14 September 2012, 2012.
[18]
N. Glodic et al., "Aeroelastic Properties of Combined Mode Shapes in an Oscillating LPT Cascade," in 12th ISUAAAT Symposium. London, UK. September 1-4, 2009, 2009.
[19]
D. Vogt, N. Glodic and T. Fransson, "The Effect of Unsteady Aerodynamic Asymmetric Perturbations on the Mode Shape Sensitivity of an Oscillating LPT Cascade," in 12th ISUAAAT Symposium. London, UK. September 1-4, 2009, 2009.
Non-peer reviewed
Theses
[20]
N. Glodic, "Sensitivity of Aeroelastic Properties of an Oscillating LPT Cascade," Licentiate thesis Stockholm : KTH Royal Institute of Technology, Trita-KRV, 13:05, 2013.
Other
[21]
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2024-11-20 01:02:42