Table 10 Flow conditions for experiment of compressor cascade.
From: High-Reynolds-Number Turbulence Database: AeroFlowData
Cases | Flow Conditions |
|---|---|
A1 compressor blade | Ma = 0.5/0.6/0.7, Re = 7.16 × 105, α = −2.5/0/2.5/5/7.5° |
A2 compressor blade | Ma = 0.5/0.6/0.71, Re = 9.2 × 105, α = −8/−4/0/4/8° |
