Thin airfoil theories of an ejector flapped wing section are reviewed. The global matching of the external airfoil flow with the ejector internal flow and the overall ejector flapped wing section aerodynamic performance are examined. Mathematical models of the external and internal flows are presented. The delineation of the suction flow coefficient characteristics are discussed. The idealized lift performance of an ejector flapped wing relative to a jet augmented flapped wing are compared.
Internal-external flow integration for a thin ejector-flapped wing section
1979-09-01
Conference paper
No indication
English
Thin-Airfoil Theory of an Ejector-Flapped Wing Section
AIAA | 1975
|Thin-airfoil theory of an ejector-flapped wing section
AIAA | 1974
|Parametric Design Study for a Blown Flapped Wing
AIAA | 2021
|Computation of Three-Dimensional Jet-Flapped Wing in Viscous Flow
Online Contents | 1996
|A lifting line theory of the jet flapped wing
TIBKAT | 1960
|