Turbulence Amplification with Incidence at the Leading Edge of a Compressor Cascade
Detailed measurements, with a two-component laser-Doppler velocimeter and a thermal anemometer were made near the suction surface leading edge of controlled-diffusion airfoils in cascade. The Reynolds number was near 700,000, Mach number equal to 0.25, and freestream turbulence was at 1.5% ahead of...
Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
Hindawi Limited
1999-01-01
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Series: | International Journal of Rotating Machinery |
Subjects: | |
Online Access: | http://dx.doi.org/10.1155/S1023621X99000081 |