The 16th Symposium on Measuring Techniques in Transonic
and Supersonic Flow in Cascades and Turbomachines
CAMBRIDGE, UK – September 2002
Sessions
Development of High-Frequency Instrumentation
Sensor Technology and Signal Processing
Development of High Frequency Instrumentation II
Heat Transfer and Cooling Effectiveness
Design and Validation of Test Facilities
Optical Emission Tomography
P. Dunkley, M. Burnett, P.
Bryanston-Cross, E. Moll & B. Timmerman, Optical Engineering Lab,
University of Warwick. J. Black,
Strategic Research Center, Rolls-Royce Derby
Records of Unsteady Transonic Flow Past Blade Cascades by Means of Optical Methods
J.
Ulrych, J. Benetka, Aeronautical Research and
Test Institute, Prague.
P.
Šafařík, Czech Technical University
in Prague.
Reynolds Stress Measurement with a Single Component Laser Doppler Anemometer
Dynamic Analysis of a Fast Response, Air-to-Fuel Equivalence Ratio Sensor
M. J. Brear, M. Jones,
Department of Mechanical and Manufacturing Engineering, University of
Melbourne, Australia.
Accuracy of Fast-Response Aerodynamic Probes in Unsteady Turbine Flows
Precise & Rapid Unsteady Pressure Transducer Signal Processing Using a Transfer Function Modeling Technique
F.
Rottmeier, A. Bölc, LTT-ISE-STI, EPFL, Swiss
Federal Institute of Technology, CH-1015 Lausanne, Switzerland.
On The Use
of Hot Film Sensors in the Investigation of Fluid Dynamic Phenomena in the Near
Wall Region
P.
C. Griffin, M. R. D. Davies, Stokes Research Institute,
Mechanical & Aeronautical Eng. Dept., University of Limerick, Limerick, Republic of
Ireland.
A Probe for the Measurement of High-Temperature Gases
X.
Yang, R. J. Miller, H P Hodson, Whittle
Laboratory, University of Cambridge Department of Engineering.
Experiences in the Application of Intermittency Detection Techniques to Hot-Film Signals in Transitional Boundary Layers
E.
Canepa, M. Ubaldi, P. Zunino, Universita di Genova.
Tip Timing Techniques for Turbomachinery HCF Condition
Monitoring
Performance Measurements in a Transient Turbine Test Facility- Preliminary Instrumentation Development
Determination of the Mass Flow in a Compression Tube Turbine Test Rig
L. Porreca and R.
Dénos, von Karman Institute for Fluid
Dynamics, Turbomachinery and Propulsion Department, Chaussée de Waterloo, 72,
1640 Rhode Saint Genèse, Belgium.
Determination of the Efficiency of a Cooled Turbine Stage Tested in a Compression Tube Facility
L. Porreca and R. Dénos, von Karman Institute for Fluid Dynamics, Turbomachinery and Propulsion Department, Chaussée de Waterloo, 72, 1640 Rhode Saint Genèse, Belgium.
Introducing the New Virtual Four Sensor Fast Response Aerodynamic Probe (FRAP Ò)
A. Pfau, J. Schlienger, A. I. Kalfas, R. S. Abhari, Turbomachinery Laboratory, Swiss Federal Institute of Technology, Zuerich, Switzerland.
High Frequency Effects in Unsteady Entropy Measurements
Measuring 3D Flow with
a Single Pressure Transducer
Pressure measurements at a nozzle guide vane edge using embedded fibre optic sensors
M J Gander, W N Macpherson,
J S Barton, R L Reuben, J D C Jones, Heriot-Watt University, K S Chana, S J
Anderson Qinetiq, Pyestock, R Stevens, Rutherford Appleton Laboratory. T V
Jones, University of Oxford.
Pressure Sensitive Paint (PSP) and Transient Liquid Crystal Technique (TLC) for Measurements of Film Cooling Performances
Data Reduction and Thermal Product Determination for Single and Multi-Layer Thin-Film Gauges
N.
Billiard, V.
Iliopoulou, F. Ferrara, R. Dénos, Von Karman Institute for Fluid Dynamics, Turbomachinery & Propulsion Department, Chaussée de Waterloo, 72,
1640 Rhode Saint Genèse.
Experimental Technique for Evaluation of Heat Transfer Coefficients with a Thermocamera in a Plexiglas Model
P. M. Magnusson, J. Hylén,
ALSTOM Power Sweden AB,Dep. of Research &
Development,S-612 82 Finspong.
Heat Transfer Measurements on a Sidewall and Blade Surface
of a Large Scale NGV with Leakage Flow
A New Turbine Cascade for Aero-mechanical Testing
D. M.
Vogt, T. H. Fransson, The Royal Institute of
Technology, Chair of Heat and Power Technology, Stockholm, Sweden.
Reliability of Low-Speed vs High Speed Testing of LP Turbine Blade Wake Interaction
A New Test Facility for Investigating Fluid-Structure Interactions Using a Generic Model
D. Allegret-Bourdon, D. M. Vogt, T. H. Fransson, The Royal Institute of Technology, Chair of Heat and Power Technology,
Stockholm, Sweden.