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...
| Huvudupphovsmän: | , , |
|---|---|
| Materialtyp: | Artikel |
| Språk: | English |
| Publicerad: |
Hindawi Limited
1999-01-01
|
| Serie: | International Journal of Rotating Machinery |
| Ämnen: | |
| Länkar: | http://dx.doi.org/10.1155/S1023621X99000081 |