The XXVI Symposium on Measuring Techniques in Turbomachinery Transonic and Supersonic Flow in Cascades and Turbomachines
Lorenzo Ferrari
University of Pisa (DESTeC), Pisa, Italy
CFD-SUPPORTED DATA REDUCTION OF HOT-WIRE ANEMOMETRY SIGNALS FOR COMPRESSIBLE ORGANIC VAPOR FLOWS
Leander Hake, Stephan Sundermeier, Stefan aus der Wiesche, Aurélien Bienner, Xavier Gloerfelt, Camille Matar, Paola Cinnella
Muenster University of Applied Sciences, Germany
Art et Metiers Institute of Technology, France
Sorbonne University, France
FLUORESCENT PIV TECHNIQUE FOR TURBOMACHINERY FLOWS
M. Okada, J. Pinho, B. Cernat, S. Lavagnoli
Turbomachinery and Propulsion Department, von Karman Institute for Fluid dynamics, Belgium
BLADE PRESSURE LOADING AND TORQUE MEASUREMENT IN A TRANSONIC LINEAR CASCADE
Jan Lepicovsky, David Šimurda, Jindřich Hála, Petr Šidlof, Martin Štěpán
Institute of Thermomechanics, Czech Academy of Sciences, Czech Republic
Technical University of Liberec, Czech Republic
VISUALIZATION TECHNIQUES FOR SUPERSONIC BLADING DESIGN FOR ORGANIC RANKINE CYCLES
Theofilos G.Efstathiadis, Konstantinos D.Eleftheriou, Konstantinos D.Bollas, Anestis I.Kalfas
Aristotle University of Thessaloniki, Department of Mechanical Engineering, Greece
EXPERIMENTAL MONITORING OF VIBRATIONS AND THE PROBLEM OF AMPLITUDE QUANTIFICATION
Alexandra P. Schneider, Benoit Paoletti, Xavier Ottavy, Christoph Brandstetter
Univ. de Lyon, Ecole Centrale de Lyon, France
A NEW EXPERIMENTAL TEST RIG FOR PERFORMANCE ANALYSIS OF RADIAL COMPRESSORS INSIDE INNOVATIVE HEAT PUMPS
Marco Ferrando, Tommaso Reboli, Sreenath Purushothaman, Alberto Traverso, Chaitanya Halbe
Università degli Studi di Genova, Italy
Carrier Corporation, East Syracuse, USA
TEST RIG DESIGN CONSIDERATIONS TO DETECT VOLATILE ORGANIC COMPOUNDS IN AIRCRAFT CABINS
Christos P. Nasoulis, Stavroula Mantziou, Vasilis G. Gkoutzamanis, Anestis I. Kalfas
Laboratory of Fluid Mechanics and Turbomachinery
Department of Mechanical Engineering, Aristotle University of Thessaloniki, Greece
WATER-COOLED FAST-RESPONSE WALL-STATIC PRESSURE PROBES FOR HARSH COMBUSTOR ENVIRONMENT APPLICATIONS
Julien Clinckemaillie, Fabrizio Fontaneto, Jean-Louis Champion-Réaud, Éric Bouty, Carlos Mendes
Turbomachinery and Propulsion Department von Kármán Institute for Fluid Dynamics, Belgium
Safran Tech, Safran Helicopter Engines, France
INVESTIGATION OF THE SUPERSONIC FLOW PAST A WEDGE-SHAPED GEOMETRY USING PRESSURE SENSITIVE PAINTS TECHNIQUE
Jindřich Hála, David Šimurda, Jan Lepičovský, Martin Luxa
Institute of Thermomechanics of the Czech Academy of Sciences, Prague, Czech Republic
DESIGN OF A SMALL PRESSURE CHAMBER TO EVALUATE PROBE CALIBRATIONS AT VARYING REYNOLDS NUMBERS
Konstantin Speck, Christian Schäffer, Volker Gümmer
Technical University of Munich, Germany
INFRARED THERMOGRAPHY TECHNIQUES FOR BOUNDARY LAYER STATE VISUALISATION
William Davis, Nicholas R. Atkins
Whittle Laboratory, University of Cambridge, UK
TIME-RESOLVED TEMPERATURE MEASUREMENTS INSIDE A COMBUSTION CHAMBER OF A TURBOMACHINE
Jean-Louis CHAMPION-RÉAUD, Pierre-Alain LAMBERT, Carlos MENDES, Sylvain PRAT, Philippe BOUYER, Martin VILESPY
Safran-Tech, France
Safran Helicopter Engines, France
INSTRUMENTATION INTERFERENCE IN A TRANSONIC LINEAR CASCADE
G. Lopes, L. Simonassi, A.F.M. Torre, S. Lavagnoli
Turbomachinery and Propulsion Department, von Karman Institute for Fluid Dynamics, Belgium
TIME-OF-FLIGHT ESTIMATION IN ACOUSTIC PYROMETRY: SENSITIVITY TO PULSE CHARACTERISTICS
Matteo Pettinari, Lorenzo Ferrari
University of Pisa (DESTeC), Italy
LASER TRIANGULATION MEASUREMENT OF BLADE OSCILLATION IN A TRANSONIC COMPRESSOR CASCADE
Petr Šidlof, Pavel Šidlof, Martin Štěpán, David Šimurda, Jan Lepicovsky
Technical University of Liberec, NTI FM, Czech Republic
Institute of Thermomechanics, Czech Academy of Sciences, Czech Republic
HALF-SCALE TRANSONIC COMPRESSOR RAPID TESTING RIG
Tianhou Wang, James Taylor
Whittle Laboratory, University of Cambridge, UK
Two-wavelength interferometry for measurement of transonic airflow in a compressor blade cascade
Pavel Psota, Jan Kredba, Marek Stašík, Gramoz Cubreli, Vít Léd, David Šimurda
Technical University of Liberec, Faculty of Mechatronics, Informatics and Interdisciplinary Studies, Institute of New Technologies and Applied Informatics (NTI), Czech Republic
Institute of Thermomechanics of the Czech Academy of Sciences, v. v. i., Czech Republic
INSTRUMENTATION IMPROVEMENTS FOR NGV AERODYNAMIC CHARACTERIZATION AT HIGH MACH NUMBERS
Andoni Puente, Guillermo Garcia-Valdecasas
Centro de Tecnologías Aeronáuticas, Spain
ITPAero, Spain
DEEP-LEARNING BASED IDENTIFICATION OF INDUCER CAVITATION INSTABILITY
Youngkuk Yoon, Sang Hyeon Lee, Seung Jin Song
Seoul National University, South Korea
REMOTE LABORATORY EXPERIMENTS: FAN MAP GENERATION AND AIRFOIL FLOW CHARACTERIZATION
Konstantinos Eleftheriou, Theofilos Efstathiadis, Anestis I. Kalfas
Aristotle University of Thessaloniki, Greece
PROBABILISTIC APPROACH FOR CORRECTION OF FIVE HOLE PROBES: EFFECT OF MACH AND WALL INTERACTION
Lakshya Bhatnagar, Andrea Ruan, Guillermo Paniagua
Purdue University, USA
PYTHONDAQ – A PYTHON BASED MEASUREMENT DATA ACQUISITION AND PROCESSING SOFTWARE
Daniel Jäger, Volker Gümmer
Technical University of Munich, TUM School of Engineering and Design, Germany
REDESIGN OF A CLOSED-LOOP HIGH-SPEED FACILITY TO TEST DISTORTION GENERATORS
Manas Payyappalli, Elissavet Boufidi, Riccardo Toracchio, Fabrizio Fontaneto
von Karman Institute for Fluid Dynamics, Belgium
IMPROVEMENT OF MEASUREMENT ACCURACY USING BAYESIAN INFERENCE - REDUCTION OF INSTRUMENTATION EFFORT IN AN AXIAL COMPRESSOR
Gonçalo G. Cruz, Xavier Ottavy, Fabrizio Fontaneto
Ecole Centrale de Lyon, Laboratoire de Mecanique des Fluides et d’Acoustique,
von Karman Institute for Fluid Dynamics, Belgium
EVOLUTION OF A FIVE-HOLE PROBE CALIBRATION NEAR A WALL
Adrien VASSEUR, Nicolas BINDER, Jean-Louis CHAMPION, Fabrizio FONTANETO
Institut Supérieur de l’Aéronautique et de l’Espace-SUPAERO, Toulouse, France
von Karman Institute for Fluid Dynamics, Belgium
SAFRAN, France
ISAE-SUPAERO, France
Laser Doppler Anemometry technique to study the flow field in the nozzle and in the water jet of a Pelton turbine
Giuseppe Roberto Pisaturo, Francesco Fabio Nicolosi, Daniele Gusmerotti, Maurizio Righetti1 and Massimiliano Renzi
Free University of Bozen, Bolzano, Faculty of Science and Technology, Italy
A FLOW FIELD AROUND A CYLINDRICAL PROBE IN PROXIMITY TO STATOR BLADES AND ITS EFFECT ON THE MEASUREMENTS
Viacheslav A Sedunin, Liping Xu, Ilya A Kalinin, Iurii G Marchenko, Oleg V Komarov
Whittle Laboratory University of Cambridge, Cambridge, UK
Energy Institute Ural Federal University Yekaterinburg, Russia
MEASURE OF THE SOLAR FLUX CONVEYED ONTO A LAMBERTIAN TARGET BY A NOVEL BI-AXIAL FRESNEL CONCENTRATOR
Marco Antonelli, Gianluca Caposciutti
University of Pisa, Department of Energy, Systems, Territory and Constructions (D.E.S.Te.C.)
EXPERIMENTAL ANALYSIS OF PARTIAL EVAPORATION MICRO-ORC FOR LOW-TEMPERATURE HEAT RECOVERY
Saverio Ottaviano, Chiara Poletto, Andrea De Pascale, Michele Bianchi
Department of Industrial Engineering – University of Bologna, Italy
COMPRESSOR FOULING DETECTION BY IMAGE ANALYSIS
Alessio Suman, Nicola Zanini, Michele Pinelli
Department of Engineering, University of Ferrara, Italy
NITROGEN EXPERIMENTS ON A SUPERSONIC LINEAR CASCADE FOR ORC APPLICATIONS
Marco Manfredi, Andrea Spinelli, Giacomo Persico, Paolo Gaetani
Energy Department, Politecnico di Milano, Italy
SIMULTANEOUS TEMPERATURE AND CONCENTRATION CALIBRATION OF PRESSURE SENSITIVE PAINT WITH ATMOSPHERIC CALIBRATION SETUP FOR FILM COOLING EFFECTIVENESS MEASUREMENTS
Dionysis S. Chala, Anestis I. Kalfas, Alexandros Terzis, Beni Cukurel
Aristotle university of Thessaloniki, Laboratory of Fluid Mechanics and Turbomachinery, Department of Mechanical
Engineering, Greece
Technion - Israel Institute of Technology, Thermo-Fluids and Interfaces Lab,Department of Aerospace Engineering, Israel
Technion - Israel Institute of Technology, Turbomachinery and Heat Transfer Laboratory, Department of Aerospace Engineering, Israel
ESTIMATING ERROR BOUNDS OF QUANTITATIVE SCHLIEREN IMAGING FOR TURBOMACHINERY APPLICATIONS
Tsinoglou M., Kalfas A., Terzis A., Mitra A., Cukurel B.
Aristotle university of Thessaloniki, Laboratory of Fluid Mechanics and Turbomachinery, Department of Mechanical
Engineering, Greece
Technion - Israel Institute of Technology, Thermo-Fluids and Interfaces Lab,Department of Aerospace Engineering, Israel
Technion - Israel Institute of Technology, Turbomachinery and Heat Transfer Laboratory, Department of Aerospace Engineering, Israel
AN ALTERNATIVE POST-PROCESSING OF TRANSIENT LIQUID CRYSTAL EXPERIMENTS USING THE WALL TEMPERATURE GRADIENT TIME RESPONSE
Alexandros Peteinaris, Ohad Haftka, Alexandros Terzis
Thermo-Fluids & interfaces Lab, Faculty of Aerospace Engineering Technion - Israel Institute of Technology, Israel
ACOUSTIC PYROMETRY FOR FLOW VELOCITY ESTIMATION: PRELIMINARY
Gianluca Caposciutti, Lorenzo Ferrari
University of Pisa (DESTeC), Italy