Wall-Pressure Sources Near an Airfoil Trailing Edge Under Separated Laminar Boundary Layers
AIAA Journal ; 49 , 9 ; 1841-1856
01.09.2011
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Wall-Pressure Sources Near an Airfoil Trailing Edge Under Separated Laminar Boundary Layers
Online Contents | 2011
|Divergent-Trailing-Edge Airfoil
NTRS | 1988
|Flow near the trailing edge of an airfoil
AIAA | 1992
|