Universität der Bundeswehr München, Germany
Proceedings of 11th Symposium 14-15 September 1992
L. Fottner
Universität der Bundeswehr München, Germany
A Review on Advanced Methods for Cascade Testing
Ch. Hirsch
Vrije Universiteit Brussel, Belgium
3D Effects in Nominally 2D Transonic Cascades
R. Dvorak
Czechoslovak Academy of Sciences, Prague, CS
Some Practical Aspects of Cascade Testing at High Reynolds Number
G. D. Willis, A.H. Truelove
GEC Alstholm Warwick, UK
3D Pneumatic & 2D Dynamic Probes: Their Development and Subsequent Use in a Transonic Fan
M.A. Cherrett, J.D. Bryce, H.P. Hodson
Calibration, Modeling and Data Evaluation Procedures for Aerodynamic Multihole Pressure Probe Measurements on the Example of a Four Hole Probe
P. Kupferschmied, Chr. Gossweiler
ETH Zürich, Switzerland
Theoretical Determination of the Characteristics of Multi-Hole Pressure Probes Using Panel Methods
Th. Depolt, W. Koschel
RWTH Aachen, Germany
Computerized Balancing of a Wedge Shaped Probe
O. Johanßen
Universität der Bundeswehr Hamburg, Germany
Experimental Tests of Transonic Nozzles in Linear Cascades Carried out by Traversing Probe
S. Cabitza, N. Mandas
Universita di Cagliari, Italy
The Dynamic Response of Capillary Tubes for Use in Miniature Pressure Probes
D. Bohn, Th. Schnittfeld
RWTH Aachen, Germany
Aerodynamic Design Criteria for Fast Response Probes
H.J. Humm, J.I. Verdegaal
ETH Zürich, Switzerland
Experimenting with Fast Response Aerodynamic Probe Geometries
R.W. Ainsworth, A.D. Stickland
Oxford University, UK
Fast Response Aerodynamic Probe Measurements in a Turbulent Pipe Flow
Chr. Gossweiler, D. Herter, P. Kupferschmied
ETH Zürich, Switzerland
Relative Total Pressure Measurements Downstream of a Transonic Annular Cascade
C.H. Sieverding, R. Denos
VKI Brussels, Belgium
Temperature Error Compensation of a Miniature Semiconductor Pressure Transducer and First Results of Measurements Taken in a Ducted Propfan Rotor
M. Maass
DLR Köln, Germany
Unsteady Pressure Response to an Oscillating Normal Shock Wave in a Nozzle
P. Ott, A. Bölcs, T.H. Fransson
EPF Lausanne, Switzerland
The Experimental Set-Up of a Triple-Sensor Anemometry and its Controlling System at the High-Speed Cascade Wind Tunnel
D. Wunderwald, G. Wilfert, L. Fottner
Universität der Bundeswehr München, Germany
Coupled Optical Velocity and Pressure Measurements in a Supersonic Flow
G. Janssens, J. Labbe, F. Lemoine, B. Leporcq
ONERA, Chatillon, France
Boundary-Layer Separation and Transition Visualized by Liquid Crystal Coating
DLR Köln, Germany
Developments in Flow Tracing Using Miniature Lasers
R.G. Dominy
University of Durham, UK
Intra-Blade Quantitative Transonic Flow Measurements at the DRA Pyestock Isentropic Light Piston Facility Using Particle Image Velocimetry
New Developments in the Laser-2-Focus Technique for Non-intrusive Velocity Measurements in Gasturbine Components
R. Schodl, W. Förster
DLR Köln, Germany
A Study of Some Measurement Errors in L2F-VeIocimetry
F. Kost
DLR Göttingen, Germany
Optical Fibre Fabry-Perot Interferometers for Calorimetric Heat Transfer Gauges
The Automatic Numerical Processing of Interferometric Transonic Flow Measurements
AW-System - An Interactive Environment for the Evaluation of Large Time Series
D. Herter, N.O. Chrisander, Chr. Gossweiler
ETH Zürich, Switzerland
Unsteady Temperature Measurements During Surge in a Highly Loaded High Pressure Compressor
A. Michel, G. Heider, A. Heckenmüller
MTU München GmbH, Germany
Measuring Experiences with a Wet Steam Turbine
R.G. Schmidt
Universität der Bundeswehr Hamburg, Germany