von Karman Institute for Fluid Dynamics, Sint-Genesius-Rode, Belgium
PROCEEDINGS OF THE 19TH SYMPOSIUM
DEVELOPMENT OF A I-CAMERA DOPPLER GLOBAL VELOCIMETER - FIRST MEASUREMENT IN AN ROUND FREE JET -
Juliane A.C. Berthiau, Sebastien Goguey, Xavier Ottavy
PIV MEASUREMENTS OF THE VORTICAL STRUCTURES IN ROTATING CHANNELS
Alberto Di Sante, René A. Van den Braembussche, Tony Arts
PIV APPLICATION TO TRANSONIC AXIAL AND RADIAL COMPRESSORS
Tunable Diode Laser Absorption Spectroscopy and its Application in an Impulse Hypervelocity Facility
J. M. Meyers
METHODOLOGY TO IMPLEMENT PSP TECHNIQUE IN A TRANSIENT FACILITY
J. Michalek, G. Paniagua, M. Vergalla, N. Zerelli, M. Tulkens
COMBINED HIGH SPEED STEREOSCOPIC P.I.V MEASUREMENTS AND UNSTEADY PRESSURE MEASUREMENTS IN THE VANELESS DIFFUSER OF A CENTRIFUGAL PUMP.
A. Dazin- S. Coudert, P. Dupont G. Caignaerd, G. Bois
STUDY OF COHERENT STRUCTURES ΙΝ COAXIAL JΕΤ NOISE USING PARTICLE IMAGE VELOCIMETRY
Β.Η. Timmerman , P.J. Bryanston-Cross
Optical Engineering Laboratory, School of Engineering, University of Warwick
METROLOGY CONSIDERATIONS FOR CALIBRATING TURBINE TIP CLEARANCE SENSORS
Vibro-Meter SA, Fribourg, Switzerland
SINGLE BLADE TIP CLEARANCE MEASUREMENTS IN A TRANSIENT RIG
TURBOMACHINERY BLADES SPECTRAL ESTIMATION FROM TIP-TIMING DATA
ASSESSMENT OF THE REASSIGNMENT TECHNIQUE APPLIED TO VIBRATORY DIAGNOSIS ON TURBOMACHINERY
Turbomeca, Safran Group, France
SOI-CMOS MEMS WALL SHEAR STRESS SENSORS
THE CORONA MASS FLOW METER
Fredrik Laurantzon, Nils Tillmarlk and P. Henrik Alfredsson
EFFICIENCY MEASUREMENT IN THE QINETIQ TURBINE TEST FACILITY WITH TEMPERATURE DISTORTION AND SWIRL: THE MASS FLOW RATE MEASUREMENT PROBLEM
RAPID PROTOTYPING FOR WIND TUNNEL TESTING AND INSTRUMENTATION
MAIN FACTORS OF APPLICATION OF ACTIVE METHODS OF THE BOUNDARY LAYER CONTROL TO THE COMPRESSOR BLADE CASCADE FLOW
Experimental study of the efflux of an aero-engine in post-combustion regime: influence of the environmental conditions
Peter Vyvey, Walter Bosschaerts, Rolf Wagemakers
EFFECTS OF A ROTATING AERODYNAMIC PROBE ON THE FLOW FIELD OF A COMPRESSOR ROTOR
PROBES IN TRANSONIC FLOW
Friedrich Kost
DLR, Institute of Propulsion Technology, Gottingen, Germany
THREE-HOLE PRESSURE PROBES AT LARGE
ESTIMATION OF TURBULENCE BY SINGLE-SENSOR PRESSURE PROBES
Dipartimento di Energia, Politecnico di Milano, ITALY
CHARACTERIZATION AND FIRST APPLICATION OF A THIN-FILM ELECTRET UNSTEADY PRESSURE MEASUREMENT TECHNIQUE
A POST PROCESSING PROCEDURE FOR THE EVALUATION OF ADIABATIC AND OVERALL EFFECTIVENESS OF EFFUSION COOLING GEOMETRIES
Bruno Facchini, Lorenzo Tarchi, Lorenzo Toni
APPLICATION OF THE TRANSIENT HEATER FOIL TECHNIQUE FOR HEAT TRANSFER MEASUREMENTS
M. Jonsson, P. Ott
NOVEL CALIBRATION METHOD FOR AN INFRARED THERMOGRAPHY SYSTEM APPLIED TO HEAT TRANSFER EXPERIMENTS IN HOT CHANNELS
M. Ochs, A. Schulz, H.-J. Bauer
A SOFTWARE MODULE FOR CORRECTING PYROMETER MEASURED TEMPERATURES
M F.G. Cremers, R.A.Rooth
A TIME-FREQUENCY POST-PROCESSING TECHNIQUE FOR THE CHARACTERIZATION OF THE UNSTEADY PHENOMENA IN THE TURBOMACHINES
Department of Mechanical Engineering, University of Padova, Italy
AN INTEGRATED TOOL FOR TURBOMACHINERY BLADING DESIGN AND ANALYSIS
Pavlos K. Zachos, Maria Pappa, Gabriel Mansour, Ioannis Tsiafis, Anestis l. Kalfas
EVALUATION OF BLADE CASCADE CHARACTERISTICS IN EXPERIMENTS CARIED OUT WITH HUMID AIR
Némec Martin
EXPERIMENTAL SETUP FOR DETAILED SECONDARY FLOW lNVESTlGATlON ΒΥ TWO-DIMENSIONAL MEASUREMENT OF ΤΟΤΑΙ- PRESSURE LOSS COEFFlClENTS ΙΝ COMPRESSOR CASCADES
Karsten Liesner, Robert Meyer
EXPERIMENTAL INVESTIGATION ON THE NEAR-FIELD AEROACOUSTIC SOURCES OF A LOW SPEED AXIAL FAN