Publication Date:
2016-06-07
Description:
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.
Keywords:
AERODYNAMICS
Type:
NASA. Ames Res. Center Workshop on Thrust Augmenting
Format:
application/pdf
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