Comparison of Two Unsteady Intermittency Models for Bypass Transition Prediction on a Turbine Blade Profile
Work
Year: 2008
Type: article
Source: Flow Turbulence and Combustion
Cites: 29
Cited by: 11
Related to: 10
FWCI: 1.046
Citation percentile (by year/subfield): 81.7
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Sustainable Development Goal Affordable and clean energy
Open Access status: closed