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articles
1.Alexandra SCHNEIDER, Benoît PAOLETTI, Xavier OTTAVYorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png (2024).
Quantification of blade vibration amplitude in turbomachinery
Int. J. Turbomach. Propuls. Power 9, 10 (18 pages). doi:10.3390/ijtpp9010010 doi.ico openalex-16x16.png
2.Anne-Lise FIQUETorcid_16x16.png, Xavier OTTAVYorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png (2024).
UHBR open-test case fan ECL5/CATANA: non-linear analysis of non-synchronous blade vibration at part-speed conditions
J. Turbomach. 146, 071003 (8 pages). doi:10.1115/1.4064841 doi.ico openalex-16x16.png
3.Anne-Lise FIQUETorcid_16x16.png, Stéphane AUBERTorcid_16x16.png, Nicolas BUFFAZ, Agathe VERCOUTTER, Christoph BRANDSTETTERorcid_16x16.png (2022).
Trapped acoustic modes in an axial multi-stage compressor leading to non-synchronous blade vibrations
Int. J. Turbomach. Propuls. Power 7, 6 (22 pages). doi:10.3390/ijtpp7010006 doi.ico hal.ico openalex-16x16.png
4.Christoph BRANDSTETTERorcid_16x16.png, Sina STAPELFELDTorcid_16x16.png (2022).
Near-stall modelling of a pitching airfoil at high incidence, Mach number and reduced frequency
Int. J. Turbomach. Propuls. Power 7, 26 (17 pages). doi:10.3390/ijtpp7040026 doi.ico openalex-16x16.png
5.Christoph BRANDSTETTERorcid_16x16.png, Xavier OTTAVYorcid_16x16.png, Benoît PAOLETTI, Sina STAPELFELDTorcid_16x16.png (2022).
Interpretation of stall precursor signatures
J. Turbomach. 143, 121011 (13 pages). doi:10.1115/1.4051709 doi.ico openalex-16x16.png
6.Valdo PAGÈS, Pierre DUQUESNEorcid_16x16.png, Stéphane AUBERTorcid_16x16.png, Laurent BLANC, Pascal FERRAND, Xavier OTTAVYorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png (2022).
UHBR Open-Test-Case Fan ECL5/CATANA
Int. J. Turbomach. Propuls. Power 7, 17 (20 pages). doi:10.3390/ijtpp7020017 doi.ico openalex-16x16.png
7.Alexandra SCHNEIDER, Benoît PAOLETTI, Xavier OTTAVYorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png (2022).
Influence of a turbulence control screen on the aerodynamic and aeroelastic behavior of an UHBR fan
preprint . hal.ico
8.Sina STAPELFELDTorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png (2021).
Suppression of nonsynchronous vibration through intentional aerodynamic and structural mistuning
J. Turbomach. 144, 021008 (8 pages). doi:10.1115/1.4052233 doi.ico openalex-16x16.png
9.Martin RODRIGUES, Laurent SOULAT, Benoît PAOLETTI, Xavier OTTAVYorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png (2021).
Aerodynamic investigation of a composite low-speed fan for UHBR application
J. Turbomach. 143, 101004 (12 pages). doi:10.1115/1.4050671 doi.ico openalex-16x16.png
10.Anne-Lise FIQUETorcid_16x16.png, Stéphane AUBERTorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png, Nicolas BUFFAZ, Agathe VERCOUTTER (2021).
Acoustic resonance in an axial multistage compressor leading to non-synchronous blade vibration
J. Turbomach. 143, 091014 (10 pages). doi:10.1115/1.4050626 doi.ico hal.ico openalex-16x16.png
11.Christoph BRANDSTETTERorcid_16x16.png, Sina STAPELFELDTorcid_16x16.png (2021).
Analysis of a linear model for non-synchronous vibrations near stall
Int. J. Turbomach. Propuls. Power 6, 26 (14 pages). doi:10.3390/ijtpp6030026 doi.ico openalex-16x16.png
12.Sina STAPELFELDTorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png (2020).
Non-synchronous vibration in axial compressors: Lock-in mechanism and semi-analytical model
J. Sound Vib. 488, 115649 (20 pages). doi:10.1016/j.jsv.2020.115649 doi.ico hal.ico openalex-16x16.png
13.Christoph BRANDSTETTERorcid_16x16.png, Benoît PAOLETTI, Xavier OTTAVYorcid_16x16.png (2019).
Compressible modal instability onset in an aerodynamically mistuned transonic fan
J. Turbomach. 141, 031004 (11 pages). doi:10.1115/1.4042310 doi.ico hal.ico openalex-16x16.png
14.Anne-Lise FIQUETorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png, Stéphane AUBERTorcid_16x16.png, Mickaël PHILIT (2019).
Non-synchronous aeroacoustic interaction in an axial multi-stage compressor
J. Turbomach. 141, 101013 (8 pages). doi:10.1115/1.4044675 doi.ico openalex-16x16.png
15.Christoph BRANDSTETTERorcid_16x16.png, Valdo PAGÈS, Pierre DUQUESNEorcid_16x16.png, Benoît PAOLETTI, Stéphane AUBERTorcid_16x16.png, Xavier OTTAVYorcid_16x16.png (2019).
Project PHARE-2 – a high-speed UHBR fan test facility for a new open-test-case
J. Turbomach. 141, 101004 (9 pages). doi:10.1115/1.4043883 doi.ico hal.ico openalex-16x16.png
 
thèses/hdr
1.Christoph BRANDSTETTERorcid_16x16.png (2022).
Non-synchronous phenomena in turbomachines
Habilitation École centrale de Lyon
2.Anne-Lise FIQUETorcid_16x16.png (dir.: Stéphane AUBERT, Christoph BRANDSTETTER) (2021).
Analyse et modélisation de phénomènes aéroélastiques non-synchrones dans un compresseur axial multi-étages
Thèse École centrale de Lyon hal.ico
 
communications avec actes
1.Christoph BRANDSTETTERorcid_16x16.png, Valdo PAGÈS, Pierre DUQUESNEorcid_16x16.png, Benoît PAOLETTI, Stéphane AUBERTorcid_16x16.png, Xavier OTTAVYorcid_16x16.png (2018).
Project PHARE-2 – a High-Speed UHBR Fan Test Facility for a new Open-Test-Case
15th International Symposium on Unsteady Aerodynamics, Aeroacoustics & Aeroelasticity of Turbomachines, Oxford, United Kingdom. hal.ico
In: Proceedings of 15th International Symposium on Unsteady Aerodynamics, Aeroacoustics & Aeroelasticity of Turbomachines, , . hal.ico
 
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