The purpose of this study is to investigate the blade-to-blade flow in an axial compressor, providing a detailed description of the entire flow-field on multiple layers through the use of Particle Image Velocimetry (PIV). Typical problems that relate to flow seeding, light-sheet generation, and camera-laser timing control are successfully dealt with, bringing additional knowledge in the domain. An extensive data set is analyzed to obtain statistical flow information (mean and fluctuating quantities). Spatial data reconstruction procedures allow the complete planar flow distributions to be determined. The multiplanar mean velocity field constitutes the final result of a three-dimensional reconstruction of the domain geometry and the proper introduction of the available planar measurements. [S0889-504X(00)00304-4]
Skip Nav Destination
Article navigation
October 2000
Technical Papers
Experimental Investigation of the Blade-to-Blade Flow in a Compressor Rotor by Digital Particle Image Velocimetry
N. Balzani,
N. Balzani
Von Karman Institute for Fluid Dynamics, Rhode-St.-Gene`se, Belgium
Search for other works by this author on:
F. Scarano,
F. Scarano
Von Karman Institute for Fluid Dynamics, Rhode-St.-Gene`se, Belgium
Search for other works by this author on:
M. L. Riethmuller,
M. L. Riethmuller
Von Karman Institute for Fluid Dynamics, Rhode-St.-Gene`se, Belgium
Search for other works by this author on:
F. A. E. Breugelmans
F. A. E. Breugelmans
Von Karman Institute for Fluid Dynamics, Rhode-St.-Gene`se, Belgium
Search for other works by this author on:
N. Balzani
Von Karman Institute for Fluid Dynamics, Rhode-St.-Gene`se, Belgium
F. Scarano
Von Karman Institute for Fluid Dynamics, Rhode-St.-Gene`se, Belgium
M. L. Riethmuller
Von Karman Institute for Fluid Dynamics, Rhode-St.-Gene`se, Belgium
F. A. E. Breugelmans
Von Karman Institute for Fluid Dynamics, Rhode-St.-Gene`se, Belgium
Contributed by the International Gas Turbine Institute and presented at the 45th International Gas Turbine and Aeroengine Congress and Exhibition, Munich, Germany, May 8–11, 2000. Manuscript received by the International Gas Turbine Institute February 2000. Paper No. 2000-GT-55. Review Chair: D. Ballal.
J. Turbomach. Oct 2000, 122(4): 743-750 (8 pages)
Published Online: February 1, 2000
Article history
Received:
February 1, 2000
Citation
Balzani , N., Scarano , F., Riethmuller , M. L., and Breugelmans, F. A. E. (February 1, 2000). "Experimental Investigation of the Blade-to-Blade Flow in a Compressor Rotor by Digital Particle Image Velocimetry ." ASME. J. Turbomach. October 2000; 122(4): 743–750. https://doi.org/10.1115/1.1311283
Download citation file:
Get Email Alerts
Related Articles
Investigation of Blade Tip Interaction With Casing Treatment in a Transonic Compressor—Part I: Particle Image Velocimetry
J. Turbomach (January,2011)
Closure to “Discussion of ‘Comparative Studies on Short and Long Length-Scale Stall Cell Propagating in an Axial Compressor Rotor’ ” (2001, ASME J. Turbomach., 123, p. 31)
J. Turbomach (January,2001)
Related Proceedings Papers
Related Chapters
Outlook
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Pulsation and Vibration Analysis of Compression and Pumping Systems
Pipeline Pumping and Compression System: A Practical Approach, Third Edition
Pulsation and Vibration Analysis of Compression and Pumping Systems
Pipeline Pumping and Compression Systems: A Practical Approach, Second Edition