The XXV Symposium on Measuring Techniques in Turbomachinery Transonic and Supersonic Flow in Cascades and Turbomachines
Anestis Kalfas
Aristotle University of Thessaloniki, Department of Mechanical Engineering, Laboratory of Fluid Mechanics and Turbomachinery
[WITHDRAWN] SPATIAL AND TEMPORAL RESOLUTION OF A FAST-RESPONSE AERODYNAMIC PRESSURE PROBE IN GRID-GENERATED TURBULENCE
Florian M. Heckmeier, Stefan Hayböck, Christian Breitsamter
Chair of Aerodynamics and Fluid Mechanics Department of Mechanical Engineering Technical University of Munich, Germany
FIVE HOLE PROBE ERRORS CAUSED BY FLUCTUATING INCIDENCE
John Coull, Tony Dickens, Henry Ng, José Serna
University of Oxford, University of Cambridge, University of Liverpool, 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, Andreas Schwab, Victor Dubois, Rico Poser, Bernhard Weigand, Jens von Wolfersdorf
Institute of Aerospace Thermodynamics (ITLR), University of Stuttgart, Germany
INTERPRETATION OF STALL PRECURSOR SIGNATURES – STABLE INSTABILITIES
Christoph Brandstetter, Xavier Ottavy, Sina Stapelfeldt
Université de Lyon, Ecole Centrale de Lyon, CNRS, LMFA, ECULLY, France
Imperial College, Department of Mechanical Engineering, London, UK
DIRECT INDUCER CAVITATION INSTABILITY IDENTIFICATION USING HIGH SPEED VISUALIZATION
Youngkuk Yoon, Seung Jin Song
ON DIRECTIONAL SENSITIVITY OF THERMO-ANEMOMETER SPLIT-FIBER PROBES
Jan Lepicovsky
Institute of Thermomechanics,Czech Academy of Sciences, Prague, Czech Republic
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,
ACCURACY IMPROVEMENT OF THE TRANSIENT HEATER FOIL TECHNIQUE FOR HEAT TRANSFER TESTS: PRELIMINARY RESULTS
Julian Schmid, Michele Gaffuri, Alexandros Terzis, Peter Ott, Jens von Wolfersdorf
Group of Thermal Turbomachinery (GTT)EPFL, Lausanne, Switzerland
Department of Mechanical Engineering, Stanford University, USA
Institute of Aerospace Thermodynamics, University of Stuttgart, 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, Sweden
BOUNDARY LAYER STREAKS CONTROL IN BYPASS TRANSITION UTILISING PLASMA ACTUATORS
Konstantinos D. Eleftheriou, Kevin Gouder, Jonathan Morrison
Department of Mechanical Engineering, Aristotle University of Thessaloniki, Greece
Department of Aeronautics, Imperial College London, UK
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, Czech Republic
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
Kempten University of Applied Sciences, Germany
INFLUENCE OF EMITTER-RECEIVER NUMBER ON MEASUREMENT ACCURACY IN ACOUSTIC PYROMETRY
L. Ferrari, G. Caposciutti, G. Pasini, G. F. Frate, U. Desideri
University of Pisa (DESTeC), Pisa, Italy
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
EFFECT OF HEATING ON THE STABILITY OF THE THREE-DIMENSIONAL BOUNDARY LAYER FLOW OVER A ROTATING DISK
Stefan aus der Wiesche, Christian Helcig
Muenster University of Applied Sciences Department of Mechanical Engineering,
Technical University of Munich Department of Aerospace and Geodesy, Germany
IMPROVING GAS TURBINE EXPERIMENTS THROUGH ADDITIVELY MANUFACTURED INSTRUMENTATION
Tamara Guimarães
Vectoflow GmbH, Penn State University, Germany
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
DESIGN OPTIMIZATION OF A NOVEL ORIFICE CONTROL VALVE FOR TURBOMACHINERY TESTING FACILITIES
Alexandros Peteinaris, Anestis Kalfas
Laboratory of Fluid Mechanics & Turbomachinery, Department of Mechanical Engineering, Aristotle University of Thessaloniki, Greece
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
ON THE APPLICATION OF BAYESIAN INFERENCE FOR AXIAL COMPRESSOR PERFORMANCE ASSESSMENT
Gonçalo G. Cruz, Fabrizio Fontaneto
von Karman Institute for Fluid Dynamics Rhode-St-Genèse, Belgium
NON-INVASIVE LEAKAGE DETECTION & LOCALISATION TECHNIQUE IN NOISY INDUSTRIAL ENVIRONMENT
Theofilos Efstathiadis, Anestis Kalfas, Georgios P. Kousiopoulos, Georgios N. Papastavrou
Department of Mechanical Engineering, Laboratory of Fluid Mechanics and Turbomachinery, Aristotle University of Thessaloniki
Department of Electronics and Computers, School of Physics, Faculty of Sciences, Aristotle University of Thessaloniki, Greece