DIEF Dipartimento di Ingegneria Industriale Univerista Degli Studi Firenze, Italy
Proceedings of the X V th Bi-Annual Symposium on Measuring Techniques in transonic and Supersonic Flows in Cascades and Turbomachines. 21-22 September 2000, Firenze/ltaly
Operation and Preliminary Measurements from a New Transonic Wind Tunnel
Mark Davies, Eamon Breathnach
Using Optical Methods in High-Speed Aerodynamic Research
Application of a Particle Image Velocimetry (PIV) System to the Periodic Unsteady Flow Around an Isolated Compressor Blade
A. Lehr, A. Bölcs
Redesign and taking into service of a new test facility for nozzle flow experiments
The new steam tunnel of the Belgian Royal Military Academy
W. Bosschaerts, Prof
KMS-ERM / MRTM, Brussels, Belgium
A Turbine Test Facility for Aerodynamic Testing
NUMERICAL COMPENSATION IN THE TIME DOMAIN OF PRESSURE SENSORS
G. Paniagua, R. Dénos
The Aerodynamic Design and use of Multi-Sensor Pressure Probes for MEMS Applications
H. Babinsky, U. Kuschel, H. P. Hodson, D. F. Moore and M. E. Welland
Optical Correction of Distortions created by Curved Window for L2F or LDA, 2D or 3D Anemometer Measurements in Turbomachine
D.ARNAUD et A.VOUILLARMET
Pressure Sensitive Paint measurements at a Transonic Compressor stage
High frequency blade surface temperature determination using surface mounted hotfilm gauges
Maik Tiedemann
GLUE-ON HOT FILM SENSORS TO INVESTIGATE HEAT TRANSFER ON A HIGHLY LOADED LP FILM COOLED TURBINE BLADE
Stefan Wolff, Leonhard Fottner
Flow conditions in a side channel compressor
Dipl.-lng. A. Krake, Univ. Prof. Dr.-Ing. K. Fiedler
Application of Three Dimensional Laser-Two-Focus Anemometry to Unsteady Flow in a Transonic Turbine Stage
A COUPLED STEADY-UNSTEADY-STATE DATA ACQUISITION SYSTEM FOR THE INVESTIGATION OF ROTATING INLET DISTORTIONS AT A MULTI-STAGE COMPRESSOR TEST FACILITY
Thomas Peters, Leonhard Fottner
A New Method for the Calibration of the Directional Sensitivity of X-Hot-Wire Probes
FABRICATION AND CALIBRATION TECHNIQUES FOR TURBINE ROTOR TIP HEAT TRANSFER GAUGES
STEVEN J. THORPE, SHIN YOSHINO & ROGER W. AINSWORTH
Aerodynamic Loss Measurements in a Linear Cascade with Film Cooling Injection
H. Reiss, A. Bölcs
HOT WIRE ANEMOMETRY AT HP ROTOR EXIT IN SUPPORT OF TRENT 500 MODEL HP TURBINE RIG TEST
R.D.Stevenson
INFLUENCE OF TEMPERATURE TRANSIENTS AND CENTRIFUGAL FORCE ON FAST RESPONSE PRESSURE TRANSDUCERS
R. Dénos, E. Valenti
FAST RESPONSE PRESSURE TRANSDUCERS FOR THE INVESTIGATION OF WAKE-INDUCED TRANSITION ON A HIGHLY LOADED LP TURBINE
Peter Stadtmüller, Leonhard Fottner
DEVELOPMENT AND FIRST APPLICATION OF A SINGLE HOLE FAST RESPONSE PRESSURE PROBE
G. Barigozzi, V. Dossena, P. Gaetani
A Study of the Frequency Response of a Micro Machined Shear-Stress Sensor Based on Thin Film Anemometry
S. Gjerstad S, Y. Fu, H.P. Hodson , W.N. Dawes and D.F. Moore
Cambridge University, Department of Engineering UK
DYNAMIC PRESSURE SENSORS: FREQUENCY RESPONSE INVESTIGATION ΑΝD CALIBRATION METHODOLOGIES
Development of Single- and Multi-Hole Fast Response Pressure Probes for Turbomachinery Applications
J. F. Brouckaert
Development of Single Sensor Fast Response Pressure Probes
Aerodynamic Influence Coefficients on an Oscillating Turbine Blade in Three-Dimensional High Speed Flow Design of a New Annular Sector Cascade Test Rig at KTH
Vogt, D. M., Fransson, T. H.
Experimental Investigation of the Periodicity in a Sector of an Annular Turbine Cascade
Acceleration Insensitive Semiconductor Pressure Sensors For High Bandwidth Measurements On Rotating Turbine Blades
A.D. Kurtz , R. W. Ainsworth , S.J. Thorpe , and A. Ned
A two-stage low pressure gas-turbine model for rotor-stator aerodynamic interaction investigations
A. Amone, A.Cattanei, F.Nurzia , R. Pacciani, P. Zunino
A New Test Facility for Probe Calibration - Offering Independent Variation of Mach and Reynolds Number
P.-A. Gieß, H.-J. Rehder, F. Kost
A Detailed Investigation of the Transitional Boundary Layer on the Suction Side of a Turbine Blade
Ugo Campora, Ferruccio Pittaluga, Marina Ubaldi, Pietro Zunino