KTH Royal Institute of Technology, Stockholm, Sweden
The 17th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines was held on Sept 9-10, 2004, at KTH, Stockholm, Sweden.
Torsten Fransson
KTH, Stockholm, Sweden
The European Virtual Institute for Gas Turbine Instrumentation (EVI-GTI)
Paul Ivey
DATA REDUCTION METHOD FOR THREE-DIMENSIONAL TRANSONIC FLOW MEASUREMENTS
P.Šafařik, M.Luxa, J.Benetka, J.Michàlek
A NEW TEST FACILITY FOR EVALUATION OF PARAMETERS DEFINING NOZZLE GUIDE VANE ENDWALL HEAT TRANSFER
PRELIMINARY STEPS IN THE DEVELOPMENT OF DOPPLER GLOBAL VELOCIMETRY AT VKI
PDA AND PIV MEASUREMENTS IN A TWO-PHASE-FLOW TRANSONIC CASCADE WIND-TUNNEL
AN OPTICAL TIME RESOLVED MULTIPLE-PULSE PIV DIAGNOSTIC FOR VISUALISING TURBULENT STRUCTURES IN HIGH SPEED AIRFLOWS
P.J. Bryanston-Cross, B.H. Timmerman, P. Dunkley, A.J. Skeen
Optical Engineering Laboratory, University of Wamick, UK
COMPOSED OPTICAL RECORDS TECHNIQUE
HIGH-SPEED DIGITAL SHADOWGRAPHY FOR HIGH-FREQUENCY SHOCK TRACKING IN SUPERSONIC FLOWS
CALIBRATION AND USE OF PRESSURE SENSITIVE PAINT (PSP) FOR A TRANSONIC FLOW APPLICATION
Nils Tillmark and P. Henrik Alfredsson
KTH Mechanics, Stockholm, Sweden
Experimental techniques used in the NASA GRC Transonic Flutter Cascade
Jan Lepicovsky
QSS, NASA GRC Cleveland, OH
DEVELOPMENT OF A THREE-COMPONENT DOPPLER GLOBAL VELOCIMETRY SYSTEM
LASER 2 FOCUS (L2F) MEASUREMENT OF INLET AND OUTLET BOUNDARY LAYER IN THE VM 100 WINDTUNNEL
Alexandros Kessar, Jiasen Hu, Torsten Fransson
IMPROVED RUGGEDISED HIGH TEMPERATURE PRESSURE TRANSDUCERS FOR GAS TURBINE ENGINE & COMPONENT RIG RESEARCH & DEVELOPMENT
A TECHNIQUE FOR USING RECESSED-MOUNTED PRESSURE TRANSDUCERS TO MEASURE UNSTEADY PRESSURE
Experimental techniques used in the NASA GRC Transonic Flutter Cascade
Jan Lepicovsky
QSS, NASA GRC Cleveland, OH
HEAT TRANSFER MEASUREMENTS AT A HIGH PRESSURE TURBINE SHROUD
Bart van Duikeren
DEVELOPMENT OF HIGH RESPONSE PRESSURE PROBES FOR TIME- RESOLVED 2D AND 3D FLOW MEASUREMENTS IN TURBOMACHINES
Dipartimento di Energetica, Politecnico di Milano, ITALY
PROBE MEASUREMENT ERRORS CAUSED BY SHEAR FLOWS
A. Appukuttan, R. J. Miller, H. P. Hodson
FLOW ADAPTIVE AERODYNAMIC PROBE FOR TURBOMACHINERY FLOWS
C. Lenherr, M. Oschwald, A.I. Kalfas, R.S. Abhari
SHAFT POWER MEASUREMENTS IN A TRANSIENT TURBINE TEST FACILITY
A NEW EXPERIMENTAL TECHNIQUE FOR MEASUREMENT OF THE STEADY-STATE METAL TEMPERATURE DISTRIBUTIONS OF FILM-COOLED NGVs
T. Povey T.V. Jones M.L.G. Oldfield