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Internal-external flow integration for a thin ejector-flapped wing sectionThin 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.
Document ID
19800001874
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Woolard, H. W. (Air Force Flight Dynamics Lab. Wright-Patterson AFB, OH, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1979
Publication Information
Publication: NASA. Ames Res. Center Workshop on Thrust Augmenting
Subject Category
Aerodynamics
Accession Number
80N10113
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19800001868Collected WorksWorkshop on Thrust Augmenting Ejectors
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