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Advanced measurement techniques for aero engines and stationary gas turbines

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VKI LS 2004-04, Advanced measurement techniques for aero engines and stationary gas turbines, ISBN 2-930389-53-2

Advanced measurement techniques for aero engines and stationary

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Advanced measurement techniques for aero engines and stationary gas turbines
March 1-5, 2004; C.H. Sieverding & J.-F. Brouckaert
  • ROBERTS, J.P. - Rolls-Royce plc, United Kingdom
    Requirements for instrumentation technology for gas turbine propulsion systems
  • BUCHLIN, J.-M. – von Karman Institute, Belgium
    Infrared thermography
  • BIRD, C. - Rolls-Royce plc, United Kingdom
    Radiation thermometry - Application to turbomachinery
  • HEYES, A.L. – Imperial College London, United Kingdom
    Thermographic phosphor thermometry for gas turbines
  • GRISCH, F. – ONERA, France
    Overview of optical diagnostics for application in turbomachinery
    Non-intrusive temperature measurements in a transonic axial compressor using spontaneous rotational Raman scattering
  • BELL, J.H. – NASA Ames Research Center, CA, USA
    Basic principles of pressure and temperature sensitive paints (PSP & TSP)
    Data acquisition and reduction with PSP and TSP
  • BENCIC, T.J. – NASA Glenn Research Center, OH, USA
    Practical examples for pressure and Temperature-Sensitive Paints measurements
  • BENCIC, T.J.1; BELL, J.H.2; SCHAIRER, E.2; GREGORY, J.3 - 1NASA Glenn Research Center, OH, USA & 2NASA Ames Research Center, CA, USA & 3Purdue University, IN, USA
    Time-resolved measurements with pressure and temperature-sensitive paints
  • KURTZ, A.D.1; CHIVERS, J.W.H.1; NED, A.A.1; GOODMAN, S.1; EPSTEIN, A.H.2; BEHEIM, G.3- 1Kulite Semiconductor Products, Inc., USA & 2Massachusetts Institute of Technology, USA & 3NASA Glenn Research Center, USA
    Improved ruggedised high temperature pressure transducers for gas turbine research, development & active gas turbine control
  • KURTZ, A.D.1; CHIVERS, J.W.H.1; NED, A.A.1; AINSWORTH, R.W.2; THORPE, S.J.2- 1Kulite Semiconductor Products, Inc., USA & 2The University of Oxford, United Kingdom
    Acceleration insensitive pressure sensors for high bandwidth measurements in high acceleration environments
  • CHANA, K.S. – QinetiQ, United Kingdom
    Requirements for instrumentation technology for gas turbine propulsion systems
    Gas total and surface temperature measurements for Harsh environments
    Time resolved pressure measurements in component test facilities and gas turbines
    Advanced measuring techniques for aero engines and stationary gas turbines
  • OBERTACKE, R. – Siemens Power Generation, Germany
    Overview on industrial gas turbine probing – The Siemens Power Generation gas turbine test bed in Berlin
    Instrumentation and routing examples in industrial gas turbines

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Manufacturer von Karman Institute for Fluid Dynamics

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