XXVI Biennial Measuring Techniques in Turbomachinery Transonic and Supersonic Flow in Cascades and Turbomachines
Lorenzo Ferrari
University of Pisa, DESTEC (Department of Energy, Systems, Territory and Construction Engineering), 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, 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 Efstathiadis, Anestis Kalfas
Department of Mechanical Engineering, Laboratory of Fluid Mechanics and Turbomachinery, Aristotle University of Thessaloniki, Greece
EXPERIMENTAL MONITORING OF VIBRATIONS AND THE PROBLEM OF AMPLITUDE QUANTIFICATION
Alexandra P. Schneider, Benoit Paoletti, Xavier Ottavy, Christoph Brandstetter
Université de Lyon, Ecole Centrale de Lyon, CNRS, LMFA, UMR 5509, France
A NEW EXPERIMENTAL TEST RIG FOR PERFORMANCE ANALYSIS OF RADIAL COMPRESSORS INSIDE INNOVATIVE HEAT PUMPS
Marco Ferrando, Tommaso Reboli, Alberto Traverso
University of Genoa, Italy
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
COOLED FAST-RESPONSE STATIC PRESSURE PROBES FOR HARSH ENVIRONMENT APPLICATIONS
Julien Clinckemaillie, Fabrizio Fontaneto
von Karman Institute for Fluid Dynamics, Belgium
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
Chair of Turbomachinery and Flight Propulsion (LTF), Technical University of Munich, Germany
AN APPROACH FOR DIGITALIZED OIL-FLOW VISUALIZATION IN THE LARGE SCALE TURBINE RIG (LSTR)
Jeannette Kruppa, Johannes Eitenmüller, Dominik Ade, Sebastian Leichtfuß, H.-P. Schiffer
INFRARED THERMOGRAPHY TECHNIQUES FOR BOUNDARY LAYER STATE VISUALISATION
William Davis, Nick Atkins
University of Cambridge, UK
TIME-RESOLVED TEMPERATURE MEASUREMENT INSIDE A COMBUSTOR CHAMBER OF A TURBOMACHINE – COMPARISON WITH LES CALCULATION
Jean-Louis CHAMPION-RÉAUD, Stéphane RICHARD, Quentin BOUYSSOU, Guillaume COTTIN, Martin VILESPY, Pierre-Alain LAMBERT, Carlos MENDES, Sylvain PRAT, Philippe BOUYER
Safran Helicopter Engines, Safran-Tech, UK
INSTRUMENTATION INTERFERENCE IN TRANSONIC LINEAR CASCADES
G. Lopes, L. Simonassi, A.F.M. Torre, S. Lavagnoli
Turbomachinery and Propulsion Department, von Karman Institute for Fluid Dynamics, Belgium
DATA ACQUISITION, CONTROL AND PROCESSING OF THE PURDUE EXPERIMENTAL AEROTHERMAL LABORATORY
Lakshya Bhatnagar, Guillermo Paniagua, Papa Aye N. Aye-Addo
Purdue Experimental Aerothermal Laboratory, Purdue University, France
TIME OF FLIGHT ESTIMATION IN ACUSTIC PYROMETRY: SENSITIVITY TO PULSE CHARACTERISTICS
Lorenzo Ferrari, Matteo Pettinari
University of Pisa (DESTeC) Department of Energy, Systems, Territory and Construction Engineering, 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, Czech Republic
Institute of Thermomechanics, Czech Academy of Sciences, Czech Republic
EXPERIMENTAL INVESTIGATION OF TRANSIENT TEMPERATURE FLUCTUATIONS IN A HIGH-SPEED RESEARCH COMPRESSOR USING HOT-WIRE ANEMOMETRY AND ITS CHALLENGES
Christian Schäffer, Alexander Rabl, Christian Helcig, Volker Gümmer
TUM School of Engineering and Design, Technische Universität München, Germany
HALF-SCALE TRANSONIC COMPRESSOR RAPID TESTING RIG
Tianhou Wang, James Taylor
TWO-WAVELENGTH INTERFEROMETRY FOR MEASUREMENT OF TRANSONIC AIRFLOW IN A COMPRESSOR BLADE CASCADE
Pavel Psota, Jan Kredba, Marek Stašík, Gramoz Cubreli, Vít Lédl, 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, Czech Republic
INSTRUMENTATION IMPROVEMENTS FOR NGV AERODYNAMIC CHARACTERIZATION AT HIGH MACH NUMBERS
Andoni Puente, Guillermo García-Valdecasas
Centro de Tecnologías Aeronáuticas, ITPAERO, Italy
DEEP-LEARNING BASED IDENTIFICATION OF INDUCER CAVITATION INSTABILITY
Youngkuk Yoon, Sang Hyeon Lee, Seung Jin Song
Department of Mechanical Engineering, Seoul National University, South Korea
REMOTE LABORATORY EXPERIMENTS: FAN MAP GENERATION AND AIRFOIL FLOW CHARACTERIZATION
Konstantinos Eleftheriou, Theofilos Efstathiadis, Anestis I. Kalfas
Department of Mechanical Engineering, Laboratory of Fluid Mechanics and Turbomachinery, Aristotle University of Thessaloniki, Greece
PROBABILISTIC APPROACH FOR CORRECTION OF FIVE HOLE PROBES: EFFECT OF MACH AND WALL INTERACTION
Lakshya Bhatnagar, Guillermo Paniagua, Andrea Ruan
Purdue University, France
PYTHONDAQ – A PYTHON BASED MEASUREMENT DATA ACQUISITION AND PROCESSING SOFTWARE
Daniel Jäger
Technical University of Munich, Germany
DESIGN OF A CLOSED-LOOP HIGH-SPEED FACILITY TO TEST DISTORTION SCREENS
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, France
von Karman Institute for Fluid Dynamics, Belgium
EVOLUTION OF A FIVE-HOLE PROBE CALIBRATION NEAR A WALL
Adrien VASSEUR
Institut Supérieur de l’Aéronautique et de l’Espace-SUPAERO, Toulouse, France
von Karman Institute for Fluid Dynamics, Rhode-Saint-Genese, Belgium
SAFRAN, Magny-les-Hameaux, France
Laser doppler velocimetry technique to study the flow field in the nozzle and in the water jet of a Pelton turbine
Massimiliano Renzi, Giuseppe Pisaturo, Francesco Nicolosi, Maurizio Righetti
University of Bozen//Bolzano, Faculty of Science and Technology
MEASUREMENT CORRECTIONS DURING SPANWISE TRAVERSING IN MULTISTAGE INDUSTRIAL COMPRESSORS
V.A Sedunin, L.Xu
University of Cambridge, UK
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
Maria Alessandra Ancona, Michele Bianchi, Lisa Branchini, Andrea De Pascale, Francesco Melino, Saverio Ottaviano, Antonio Peretto, Chiara Poletto
Department of Industrial Engineering (DIN) – University of Bologna, Italy
COMPRESSOR FOULING DETECTION BY IMAGE ANALYSIS
Alessio Suman, Nicola Zanini, Michele Pinelli
THERMAL PERFORMANCE INVESTIGATION OF METAL FOAM HEAT EXCHANGER FOR MICRO-GAS TURBINE
Panagiota Chatzi, Antonia Antoniadou, Theofilos Efstathiadis, Anestis Kalfas
Department of Mechanical Engineering, Aristotle University of Thessaloniki, Greece
NOVEL STABILITY IDENTIFICATION METHOD FOR TURBOMACHINERY APPLICATED SCHLIEREN SYSTEMS
Michail Tsinoglou, Anestis Kalfas, Beni Cukurel, Abhijit Mitra, Alexandros Terzis
Aristotle University of Thessaloniki, Laboratory of Fluid Mechanics and Turbomachinery
Technion - Israel Institute of Technology, Turbomachinery and Heat Transfer Laboratory
Technion - Israel Institute of Technology, Thermo-Fluids and Interfaces Laboratory
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
ACOUSTIC PYROMETRY FOR FLOW VELOCITY ESTIMATION: PRELIMINARY ANALYSIS
Lorenzo Ferrari, Gianluca Caposciutti
DESTeC, University of Pisa, Italy
SIMULTANEOUS TEMPERATURE AND CONCENTRATION CALIBRATION OF PRESSURE SENSITIVE PAINT 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,
Technion - Israel Institute of Technology, Thermo-Fluids and Interfaces Lab, Department of Aerospace Engineering,
Technion - Israel Institute of Technology, Turbomachinery and Heat Transfer Laboratory, Department of Aerospace Engineering,