Laser Doppler Anemometry Measurements in an Axial Compressor Stage

The aim is to provide unsteady experimental data on the flowfield in a benchmark one-stage axial compressor, to improve the understanding of the flow features. The investigation is conducted with a two-component LDA, and 32 axial locations are surveyed, from the rotor inlet to the stator outlet. Bec...

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Bibliographische Detailangaben

Veröffentlicht in:	Journal of propulsion and power 2001-05, Vol.17 (3), p.481-491
Hauptverfasser:	Faure, Thierry M, Michon, Guy-Jean, Miton, Hubert, Vassilieff, Nicolas
Format:	Artikel
Sprache:	eng
Schlagworte:	Anemometers Axial flow Boundary layers Compressors Doppler effect Fluid mechanics Laser beams Mechanics Physics Rotors Turbocompressors Turbomachine blades Velocity measurement Vortex flow Wakes
Online-Zugang:	Volltext
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