Loukas and Evangelou Bellonia Foundation
The 25th Symposium on Measuring Techniques in Turbomachinery Transonic and Supersonic Flow in Cascades and Turbomachines to be held on September 21-23, 2020, Loukas and Evangelou Bellonia Foundation, Santorini, Greece
Prof. Anestis Kalfas
Aristotle University of Thessaloniki, Department of Mechanical Engineering, Laboratory of Fluid Mechanics and Turbomachinery
BLADE HEALTH MONITORING FOR FAILURE PREVENTION AND OPERATIONS INTELLIGENCE
Kamel-Abdelkader Tayebi, Bakr Alshehri, Abdurrahman Khalid, Baker Hughes
Affiliation
Ceneral Electric Power
PNEUMATIC AVERAGING ERRORS OF MULTI-HOLE PROBES IN UNSTEADY FLOW
John Coull, Tony Dickens, Henry Ng
University of Oxford, University of Cambridge, University of Liverpool, UK
ON THE APPLICATION OF BAYESIAN INFERENCE FOR TURBOMACHIENRY COMPONENTS ASSESMENT
Gonçalo G. Cruz, Fabrizio Fontaneto
Von Karman Institute for Fluid Dynamics
A NEW TEST FACILITY FOR ADVANCED TESTING OF VARIABLE INLET GUIDE VANES
Roman Frank, Christian Wacker, Reinhard Niehuis
Institute of Jet Propulsion Bundeswehr University Munich, MAN Energy Solutions Berlin
DESIGN OF A HIGH-TEMPERATURE TEST FACILITY TO STUDY THE IMPACT OF TEMPERATURE RATIO ON COOLING PERFORMANCE
Aravin Dass Naidu, Thomas Povey
A WIND TUNNEL TO ASSESS THE PERFORMANCE OF INERTIAL PARTICLE SEPARATORS FOR TURBO-PROF AND TURBO-SHAFT ENGINES
S. Castegnaro, F. Fontaneto
“Jacques Chauvin” Laboratory, von Karman Institute for Fluid Dynamics, Belgium
ON DIRECTIONAL SENSITIVITY OF THERMO-ANEMOMETER SPLIT-FIBER PROBES
Jan Lepicovsky
Institute of Thermomechanics, Czech Academy of Sciences, Prague, Czech Republic
INTERPRETATION OF STALL PRECURSOR SIGNATURES
Christoph Brandstetter, Xavier Ottavy, Sina Stapelfeldt
Ecole Centrale de Lyon, Laboratoire de Mecanique des Fluides et d’Acoustique, Lyon, France
Imperial College, Department of Mechanical Engineering, London, United Kingdom
SHOCK WAVE BOUNDARY LAYER INTERACTION MEASURED BY PIV AND HIGH-SPEED SCHLIEREN ON THE SUCTION SIDE OF A TRANSONIC TURBINE CASCADE
Marcel Börner, Reinhard Niehuis
Institute of Jet Propulsion, Bundeswehr University Munich, Germany
COOLED FAST-RESPONSE PRESSURE PROBES DESIGN METHODOLOGY FOR HARSH ENVIRONMENT APPLICATIONS
Julien Clinckemaillie, Fabrizio Fontaneto
von Karman Institute for Fluid Dynamics, Belgium
SPATIAL AND TEMPORAL RESOLUTION OF A FAST-RESPONSE AERODYNAMIC PRESSURE PROBE IN GRID-GENERATED TURBULENCE
Florian M. Heckmeier, Stefan Hayböck, Christian Breitsamter
NON-AXISYMMETRIC COMPLETE FLOW CONDITIONING GAUZES
Alejandro Castillo Pardo, James V. Taylor
ACCURACY IMPROVEMENT OF THE TRANSIENT HEATER FOIL TECHNIQUE FOR HEAT TRANFER TESTS: PRELIMINARY RESULTS
Julian Schmid, Michele Gaffuri, Peter Ott, Jens von Wolfersdorf
Group of Thermal Turbomachinery (GTT),EPFL- Swiss Federal Institute of Technology, Lausanne, Switzerland
Institute of Aerospace Thermodynamics, University of Stuttgart, Germany
[WITHDRAWN] - MINIMISING ERRORS FROM BINARY PRESSURE SENSITIVE PAINT
Joao Vieira, Peter Ireland, Mark Quinn, John Coull, Holt Wong
University of Oxford, Oxford, UK
University of Manchester, Manchester, UK
CONDUCTION AND INERTIA CORRECTION FOR TRANSIENT THERMOCOUPLE MEASUREMENTS. PART II: EXPERIMENTAL VALIDATION AND APPLICATION
Tobias Krille, Rico Poser, Markus Diel, Jens von Wolfersdorf
Institute of Aerospace Thermodynamics (ITLR) University of Stuttgart, Germany
CONDUCTION AND INERTIA CORRECTION FOR TRANSIENT THERMOCOUPLE MEASUREMENTS. PART I: ANALYTICAL AND NUMERICAL MODELLING
Florian Seibold, Victor Dubois, Bernhard Weigand, Andreas Schwab, Rico Poser, Jens von Wolfersdorf
Institute of Aerospace Thermodynamics (ITLR) University of Stuttgart, Germany
PUT PAPER TITLE HERE EXPERIMENTAL STUDY FOR NON-INVASIVE PIPELINE LEAK DETECTION AND LOCALIZATION IN NOISY ENVIRONMENT
Theofilos Efstathiadis, Georgios N. Papastavrou, Georgios P. Kousiopoulos, Anestis Kalfas, Spiros Nikolaidis
Department of Mechanical Engineering, Laboratory of Fluid Mechanics and Turbomachinery
Department of Electronics and Computers, School of Physics, Faculty of Sciences
NEW EXPERIMENTAL CONDENSING FLOW RESULTS PERFORMED IN A BARSCHDORFF NOZZLE
Manuel E. Maqueo Martinez, Stefan Winkelmann, Markus Schatz, Damian M. Vogt
ITSM, University of Stuttgart, Germany
LSM, Helmut-Schmidt-University, Hamburg, Germany
BLADE OSCILLATION MECHANISM FOR AERODYNAMIC DAMPING MEASUREMENTS AT HIGH REDUCED FREQUENCIES
Nenad Glodic, Carlos Tavera Guerrero, Mauricio Gutierrez Salas
KTH Royal Institute of Technology
UPGRADE OF THE HIGH-SPEED CASCADE WIND TUNNEL AT THE BUNDESWEHR UNIVERSITY MUNICH
Reinhard Niehuis, Martin Bitter
Institute of Jet Propulsion, Bundeswehr University Munich, Germany
DESIGN OPTIMIZATION OF A NOVEL ORIFICE CONTROL VALVE FOR TURBOMACHINERY TESTING FACILITIES
Alexandros Peteinaris, Anestis Kalfas
DEVELOPMENT OF FAST-RESPONSE MULTI-HOLE PROBES FOR AERODYNAMIC MEASUREMENTS IN TURBOMACHINERY
B. Cernat, S. Marzullo, S. Lavagnoli
von Karman Institute for Fluid Dynamics, Brussels, Belgium
DEVELOPMENT OF A FAST-RESPONSE TOTAL TEMPERATURE PROBE FOR SHORT-DURATION TURBINE RIGS
G. Luppino, B. Cernat, S. Lavagnoli
HIGH-ACCURACY INFRARED MEASUREMENTS IN THE OXFORD TURBINE RESEARCH FACILITY: CALIBRATION AND ERROR EVALUATION METHODS
Manuela Sisti, Chiara Falsetti, Kam S. Chana, Paul F. Beard
Oxford Thermofluids Institute University of Oxford, UK
TURBOCOMPRESSOR TEST FACILITY OPERATING WITH HELIUM-NEON GAS MIXTURES OF VARYING MIXING RATIOS
Maxime Podeur, Damian M. Vogt
University of Stuttgart, Germany
ON PIEZOELECTRIC ENERGY HARVESTING FOR AUTONOMOUS SENSING IN TURBOMACHINERY
Antiopi-Malvina Stamatellou, Anestis I. Kalfas
Aristotle University of Thessaloniki, Greece
ENVIRONMENTAL-FRIENDLY FIRE SYSTEM FOR CARGO USING INNOVATIVE GREEN TECHNOLOGY
Diakostefanis, M., Dinesh. A., Sampath, S., Xiong, Y.
Cranfield University, UK
ON TURBULENCE MEASUREMENTS WITH MULTI-SENSOR FAST RESPONSE AERODYNAMIC PROBES IN A HIGH-PRESSURE TURBINE
A.C. Chasoglou, P. Tsirikoglou, A.I. Kalfas, R.S. Abhari
POD-BASED ANALYTICS AND PREDICTION IN SUPPORT OF THE CALIBRATION PROCESS OF FAST-RESPONSE AERODYNAMIC PROBES
P. Tsirikoglou, A. C. Chasoglou, A. I. Kalfas, R. S. Abhari
EXPERIMENTAL INVESTIGATION OF LEAKAGE FLOW SYSTEM FOR LOW SPEED TURBINE CASCADE
Dunam Hong, Seung Jin Song
Seoul National University, South Korea
[WITHDRAWN] - NEW EXPERIMENTAL CONDENSING FLOW RESULTS PERFORMED IN A BARSCHDORFF NOZZLE
Manuel E. Maqueo Martinez, Stefan Winkelmann, Markus Schatz, Damian M. Vogt
ITSM, University of Stuttgart, LSM, Helmut-Schmidt-University Hamburg, Germany
OPTICAL AND HOT FILM MEASUREMENTS OF THE BOUNDARY LAYER TRANSITION ON A NACA AIRFOIL
David Šimurda, Jindřich Hála, Martin Luxa, Tomáš Radnic
Institute of Thermomechanics of the Czech Academy of Sciences, CR
ON DYNAMICAL STRUCTURES BEHIND A STAGE OF AN AXIAL AIR TEST TURBINE
D. Duda, V. Yanovych, V. Uruba, P. Žitek, M. Němec, T. Jelínek
University of West Bohemia in Pilsen
Czech Aerospace Research Centre in Prague
PARTICLE IMAGE VELOCIMETRY MEASUREMENT INSIDE AXIAL AIR TEST TURBINE
D. Duda, V. Yanovych, V. Uruba, P. Žitek, M. Němec, T. Jelínek
University of West Bohemia in Pilsen
Czech Aerospace Research Centre in Prague
BIOMASS WOODCHIP TRACKING BY IMAGE ANALYSIS IN A MODEL OF A FIXED BED COMBUSTOR
Lorenzo Ferrari, Gianluca Caposciutti, Martin Higl, Bernhard Müller
University of Pisa (DESTeC), Italy
INFLUENCE OF THE NUMBER OF EMITTER-RECEIVER COUPLES ON MEASUREMENT ACCURACY IN ACOUSTIC PYROMETRY
Lorenzo Ferrari, Gianluca Caposciutti
University of Pisa (DESTeC), Italy
AERODYNAMIC AND HEAT TRANSFER INVESTIGATION OF METAL FOAM FOR TURBOCHARGER OPTIMIZATION
Antonia Antoniadou, Theofilos G. Efstathiadis and Anestis I. Kalfas
Department of Mechanical Engineering, Aristotle University of Thessaloniki, Greece
BOUNDARY LAYER STREAKS CONTROL IN BYPASS TRANSITION UTILISING PLASMA ACTUATORS
Konstantinos D. Eleftheriou, Kevin Gouder, Jonathan Morrison