F. Brouckaert - the von Karman Institute for Fluid Dynamics

PUBLICATIONS (BROUCKAERT J.-F.) January 2014Archival Journal PublicationsDÉNOS, R.; SIEVERDING, C.H.; ARTS,T.; BROUCKAERT, J.F.; PANIAGUA, G.; ANDMICHELASSI, V., "Experimental Investigation of the Unsteady Rotor Aerodynamics of aTransonic Turbine Stage", Proceedings of the IMechE, Journal of Power and Energy, vol. 23,N°A4, pp327-338, 1999.SIEVERDING, C.H.; ARTS, T.; DÉNOS, R.; BROUCKAERT, J.F., "Measurement Techniquesfor Unsteady Flows in Turbomachines", Experiments in Fluids, Vol. 28, N° 4, pp 285-231, May2000.SIEVERDING, C.H.; OTTOLIA, D.; BAGNERA, C.; CIMADORO, A.; BROUCKAERT, J.-F.;DESSE, J.-M., “Unsteady turbine blade wake characteristics”, Journal of Turbomachinery, Vol.126, pp551-559, October 2004.BROUCKAERT, J.F., “Fast Response Aerodynamic Probes for Measurements in Turbomachines”,Journal of Power and Energy, Special Issue on Turbomachinery, Proc. IMechE Vol. 221 Part A,pp803-813, September 2007.VAN DEN BRAEMBUSSCHE, R.A., BROUCKAERT, J.F., PANIAGUA, G., BRIOTTET, L.,“Design and Optimization of a Multistage Turbine for Helium Cooled Reactor”, NuclearEngineering and Design, Vol. 238, pp 3136-3144, Elsevier, 2008.BROUCKAERT, J.F., MERSINLIGIL, M., PAU, M., “A Conceptual Design Study for a NewHigh Temperature Fast Response Cooled Total Pressure Probe”, GTP-08-1132, Journal ofEngineering for Gas Turbines and Power, Vol.131, No. 2, March 2009.MERSINLIGIL, M., BROUCKAERT, J.F., DESSET, J, “Unsteady Pressure Measurements with aFast Response Cooled Probe in High Temperature Gas Turbine Environments”, ASME GTP-10-1206, Journal of Engineering for Gas Turbines and Power (Vol.133, Iss.8), August 2011.MERSINLIGIL, M., DESSET, J., BROUCKAERT, J.F., “High-Temperature High-FrequencyTurbine Exit Flow Field Measurements In A Military Engine With A Cooled Unsteady TotalPressure Probe”, Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Powerand Energy (vol.225, no.7 pp.954-963), November 2011.MERSINLIGIL, M., BROUCKAERT, J.F., COURTIADE, N., OTTAVY, X., “A HighTemperature High Bandwidth Fast Response Total Pressure Probe For Measurements In AMultistage Compressor”, ASME GTP-11-1352, Journal of Engineering for Gas Turbines andPower (Vol.134, Iss.6), June 2012.MERSINLIGIL, M., BROUCKAERT, J.F., COURTIADE, N., OTTAVY, X., “On Using FastResponse Pressure Sensors In Aerodynamic Probes To Measure Total Temperature And EntropyGeneration In Turbomachinery Blade Rows”, ASME GTP-101601, Journal of Engineering for GasTurbines and Power (Vol.135, No. 10), October 2013.@von Karman Institute for Fluid Dynamics 1

SANS, J., RESMINI, M., BROUCKAERT, J.F., HIERNAUX, S., “Numerical Investigation Of TheSolidity Effect On Linear Compressor Cascades”, ASME Turbo Expo 2014, GT 2014-25532,Accepted for journal publication in Journal of Engineering for Gas Turbines and Power.Conference Papers (since 2000)Brouckaert, J.-F., 2000: "Development of Single- and Multi-Hole Fast Response Pressure Probesfor Turbomachinery Applications", 15th Symposium on Measuring Techniques for Transonic andSupersonic Flows in Cascades and Turbomachines, Firenze, Italy.Brouckaert, J.-F., 2005: “Fast Response Aerodynamic Probes for Time-Resolved Measurements inTurbomachines”, 2nd EVI-GTI International Conference on Gas Turbine Instrumentation, October12-13, 2005, Dubrovnik, Croatia, VKI RP 2006-85.Van den Braembussche, R.A.; Brouckaert, J.-F.; Paniagua, G.; Briottet, L., 2006: , “Design andoptimization of a multistage turbine for helium cooled reactor”, HTR 2006, 3rd InternationalTopical Meeting on High Temperature Reactor Technology, October 1-4, 2006, Johannesburg,South Africa, VKI RP 2007-01.Brouckaert, J.-F., 2007: “Fast Response Aerodynamic Probes for Measurements inTurbomachines”, 7th European Conference on Turbomachinery Fluid Dynamics andThermodynamics, March 5-9, 2007, Athens, Greece, VKI RP 2007-26.Moreau, S.; Henner, M.; Brouckaert, J.-F., Neal, D., 2007: “Numerical and ExperimentalInvestigation of Rotor-Stator Interaction in Automotive Engine Cooling Fan Systems”, 7thEuropean Conference on Turbomachinery Fluid Dynamics and Thermodynamics, March 5-9, 2007,Athens, Greece, VKI RP 2007-25.Hiernaux, S., de Vriendt, O., Brouckaert, J.F., Lepot, I. : “Next Generation Boosters”, Proceedingsof the 18 th ISABE Conference, Beijing, China, September 2-7, 2007.Brouckaert, J.F., Mersinligil, M., Pau, M. : “A Conceptual Design Study for a New HighTemperature Fast Response Cooled Total Pressure Probe”, 14 pages, ASME Turbo ExpoConference, Berlin, Germany, June 9-13, 2008. ASME Controls, Diagnostics & InstrumentationCommittee 2008 Best Paper Award.Brouckaert, J.F. ; Mersinligil, M. ; Pau, M.: “Development of a high temperature fast responsecooled total pressure probe”, 2nd Joint EVI-GTI / PIWG International Gas TurbineInstrumentation Conference, Seville, Spain, September 24-26, 2008.Moreau, S., Henner, M. Brouckaert, J.-F. : Comparison of experimental and numerical flow field inan automotive engine cooling module, 8 th European Turbomachinery Conference, Graz, Austria,March 23-27, 2008.B. Farkas, N. Van de Wyer, J-F. Brouckaert, R. Capart, J-F. Thomas, N. Isaac, S. Hiernaux,“Experimental and Numerical Investigation of a single Stage Low Pressure Compressor With andWithout Casing Treatment : Part 1 – Testing and Performance Verification”, VITAL Workshop,Budapest, March 9-10, 2009.@von Karman Institute for Fluid Dynamics 2

N. Van de Wyer, B. Farkas, J-F. Brouckaert, R. Capart, J-F. Thomas, N. Isaac, S. Hiernaux,“Experimental and Numerical Investigation of a single Stage Low Pressure Compressor With andWithout Casing Treatment : Part 2 – Unsteady Flow Field Analysis”, VITAL Workshop, Budapest,March 9-10, 2009.J.-F. Brouckaert, N. Van de Wyer, J. Desset, B. Farkas, J. Gonzalez Perez, R. Capart, J.-F. Thomas,N. Isaac, S. Hiernaux : Experimental and numerical investigation of a single stage Low Pressurecompressor for counter-rotating turbofan Engine architectures, 8 th European TurbomachineryConference, Graz, Austria, March 23-27, 2008.Brouckaert, J.F., Van de Wyer, N., Farkas, B., Ullmann, F., Desset, J., de Laborderie, J., Chomé,M., Hiernaux, S. Unsteady pressure measurements in a single stage low pressure axial compressor :tip vortex flow and stall inception. ASME Turbo Expo 2009, June 8-12, 2009, Orlando, Florida,USA.Mersinligil, M., Desset, J., Brouckaert, J.F., “Combustion Rig and Gas Turbine EngineMeasurements with a High Temperature Cooled Fast Response Pressure Probe”, 4th EVI-GTIInternational Gas Turbine Instrumentation Conference, Norrköping, Sweden, 2009.Brouckaert, J.F., “A New Fast Response Cooled Total Pressure Probe for Measurements in VeryHigh Temperature Gas Turbine Environments”, Ercoftac Yearly Seminar, December 3, 2009,Brussels, Belgium.Brouckaert, J.F., “Design Study and First Unsteady Measurements with a Fast Response CooledTotal Pressure Probe in Very High Temperature Gas Turbine Environments”, ETE’ 2009 SecondEUREKA International Symposium on Environmental Testing Engineering Towards aninformation exchange between Academy and Industry, 26-27 November 2009, Royal MilitaryAcademy, Brussels, Belgium.Van de Wyer N., Farkas B., Desset J., Brouckaert J.-F., Thomas J.-F., Hiernaux S., “Experimentalinvestigation of the steady and unsteady flow field in a single stage low pressure axial compressorwith a circumferential groove casing treatment.” ASME Turbo Expo 2010, Glasgow, UK.Mersinligil, M., Desset, J., Brouckaert, J.F., ”First Unsteady Pressure Measurements with a FastResponse Cooled Total Pressure Probe in High Temperature Gas Turbine Environments”, ASMETurbo Expo 2010, Glasgow, UK.Brouckaert, J.F., Mersinligil, M., Pau, M. “A Conceptual Design Study For A New HighTemperature Fast Response Cooled Total Pressure Probe", ASME GT2008-51054, Proceedings ofthe ASME Turbo Expo 2008 Power for Land, Sea and Air, June 9-13, 2008, Berlin, Germany.Mersinligil, M., Brouckaert, J.F. “A Conceptual Design Study For A New High Temperature FastResponse Cooled Total Pressure Probe”, EVI 2008-032, 2 nd Joint EVI-GTI/PIWG InternationalGas Turbine Conference, September 24-26, 2008, Seville, Spain.Brouckaert, J.F., Mersinligil, M., Desset, J., Pau, M., “High Temperature Cooled Fast ResponsePressure Probe”, in VKI LS 2009-06, “Advanced High Temperature Instrumentation for GasTurbine Applications”, May 11-14, 2009, von Karman Institute, Rhode-Saint-Genèse, Belgium.@von Karman Institute for Fluid Dynamics 3

Mersinligil, M., Brouckaert, J.F., Desset, J., “Combustion Rig and Gas Turbine EngineMeasurements with a High Temperature Cooled Fast Response Pressure Probe”, EVI 2009-009,4th EVI-GTI International Gas Turbine Instrumentation Conference, September 23-25, 2009,Norrköping, Sweden, 2009.Mersinligil, M., Brouckaert, J.F., Desset, J., “First Unsteady Pressure Measurements with a FastResponse Cooled Total Pressure Probe in High Temperature Gas Turbine Environments”, ASMEGT2010-23630, ASME Turbo Expo 2010 Power for Land Sea and Air, June 14-18, 2010,Glasgow, UK.Mersinligil, M., Brouckaert, J.F., Desset, J., “Turbine and Combustion Chamber Measurementswith a Cooled Unsteady Total Pressure Probe”, European Turbine Network, 5th International GasTurbine Conference “The Future of Gas Turbine Technology”, 27-28 October 2010, Brussels,Belgium.Brouckaert, J.F., Mersinligil, M., Desset, J. “Development and Use of a Cooled Unsteady TotalPressure Probe for Turbine and Combustion Chamber Measurements”, 3rd Joint PIWG / EVI-GTIInternational Gas Turbine Instrumentation Conference, October 26-29, 2010, Newport News, VA,USA.Mersinligil, M., Desset, J., Brouckaert, J.F., “High Temperature High Frequency Turbine Exit FlowField Measurements in a Military Engine with a Cooled Unsteady Total Pressure Probe”, 9thEuropean Turbomachinery Conference, March 21-25, 2011, Istanbul, Turkey.Mersinligil, M., Brouckaert, J.F., Courtiade, N., Ottavy, X., “A High Temperature High BandwidthFast Response Total Pressure Probe For Measurements In A Multistage Axial Compressor”, ASMEGT2011-45558, ASME Turbo Expo 2011 Power for Land Sea and Air, June 6-10, 2011,Vancouver, Canada.Mersinligil, M., Brouckaert, J.F., Courtiade, N., Ottavy, X., “On Using Fast Response PressureSensors In Aerodynamic Probes To Measure Total Temperature And Entropy Generation InTurbomachinery Blade Rows”, ASME GT2012-69722, ASME Turbo Expo 2012 Power for LandSea and Air, June 11-15, 2012, Copenhagen, Denmark.N. Van de Wyer, R. Miorini, J-F. Brouckaert, “On the determination of the transfer function ofinfinite line pressure probes for turbomachinery applications”, ASME GT2012-69722, ASMETurbo Expo 2012 Power for Land Sea and Air, June 11-15, 2012, Copenhagen, Denmark.J. Sans, J. Desset, G. Dell’Era, J.-F. Brouckaert and S. Hiernaux: «Performance testing of a lowpressure compressor» European Turbomachinery Conference 2013, Lapeenranta, Finland - April-2013.J. Sans, J.Desset, G. Dell’Era, J.-F. Brouckaert and S. Hiernaux : «Time-Resolved measurements ofthe unsteady flow field in a single stage low pressure axial compressor » ASME Turbo Expo 2013,San Antonio, TX, USA - June-2013.@von Karman Institute for Fluid Dynamics 4

Sans, J., Resmini, M., Brouckaert, J.F., Hiernaux, S., “The Impact Of Turbulence Model AndNumerical Scheme On The Performance Of A Linear Compressor Cascade”, ASME Turbo Expo2014, Düsseldorf, Germany, GT 2014-25531.Sans, J., Resmini, M., Brouckaert, J.F., Hiernaux, S., “Numerical Investigation Of The SolidityEffect On Linear Compressor Cascades”, ASME Turbo Expo 2014, Düsseldorf, Germany, GT2014-25532, Accepted for journal publication in Journal of Engineering for Gas Turbines andPower.Editor of BooksVKI LS 2004-04, Advanced measurement techniques for aero engines and stationary gas turbines.March 1-5, 2004, von Karman Institute, Rhode Saint Genese, Belgium.Sieverding, C.H.; Brouckaert, J.F.; eds.ISBN : 2930389532. \\Admin1\LIBRARY\biblio\journals\online journal\VKI LS “Data Acquisition and Signal Processing for Turbomachinery Applications.” 2005.VKI LS 2005-03, April 11-15, 2005, von Karman Institute, Rhode Saint Genese, Belgium.Brouckaert J.-F., T. Arts, (not edited).Dénos, R.; Brouckaert, J.F.; editors“Advances in Axial Compressor Aerodynamics.” 2006.VKI LS 2006-06, May 15-18, 2006, von Karman Institute, Rhode Saint Genese, Belgium.Brouckaert, J.F.; editor“Tip Timing and Tip Clearance Problems in Turbomachines.” 2007.VKI LS 2007-03, February 5-9, 2007, von Karman Institute, Rhode Saint Genese, Belgium.Brouckaert, J.F.; editor“Wind Turbine Aerodynamics, a State-of-the-Art.” 2007.VKI LS 2007-05, March 19-23, 2007, von Karman Institute, Rhode Saint Genese, Belgium.Brouckaert, J.F.; editor„Advanced High Temperature Instrumentation for Gas Turbine Applications”VKI LS 2009-06, May 11-14, 2009, von Karman Institute, Rhode Saint Genese, Belgium.NATO-RTO-Technical Report-AVT-180, “Gas Turbine Engine Test Cell Instrumentation”,STANGE W., BROUCKAERT J.-F., to be published.Contributions to booksBROUCKAERT, J.-F.:“Phase-Locked Averaging Methods for Turbomachinery Applications”, in: VKI LS 2014-01,„Advanced Post-Processing of Experimental and Numerical Data”BROUCKAERT, J.-F.:“High temperature cooled fast response pressure probe”, in: VKI LS 2009-06, „Advanced HighTemperature Instrumentation for Gas Turbine Applications”@von Karman Institute for Fluid Dynamics 5

BROUCKAERT, J.-F.:“Unsteady pressure measurements”, in: VKI LS 2008-02, Experimental determination of dynamicstability parameters, Rhode-St-Genèse, Belgium, February 18-22, 2008BROUCKAERT, J.-F.“Unsteady pressure measurements” VKI LS - Introduction to Measurement Techniques, R.A. Vanden BraembusscheSIEVERDING, C.H.; DÉNOS, R.; ARTS, T.; BROUCKAERT, J.F.; PANIAGUA, G.:“Experimental Investigation of the unsteady rotor aerodynamics and heat transfer of a transonicturbine stage”, VKI Lecture Series 1998-02 on “Blade Row Interference Effects In AxialTurbomachinery Stages”.ARTS, T.; DENOS, R.; BROUCKAERT, J.F:“Hot wire thermometry” , in: VKI Lecture Series 1996-07 on “Temperature Measurements”.@von Karman Institute for Fluid Dynamics 6