NASA NTRS · 19800001874
Internal-external flow integration for a thin ejector-flapped wing section
Abstract
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.
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Woolard, H. W.. 1979-09-01. Internal-external flow integration for a thin ejector-flapped wing section. https://ntrs.nasa.gov/citations/19800001874
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