Transition Mechanisms in Laminar Separated Flow Under Simulated Low Pressure Turbine Aerofoil Conditions
Journal of turbomachinery ; 135 , 1
2013
Article (Journal)
English
ESTABLISHMENT OF LAMINAR BOUNDARY LAYER FLOW ON AN AEROFOIL BODY
European Patent Office | 2015
|Laminar Separated Flow Nonlifting Ellipses
AIAA | 1975
|Laminar boundary layer instability noise produced by an aerofoil
Online Contents | 2009
|