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Wind-tunnel investigation of an NACA 0009 airfoil with 0.25-and 0.50-airfoil-chord plain flaps tested independently and in combination
Document ID
19930082201
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Spearman, M Leroy
Date Acquired
August 16, 2013
Publication Date
March 1, 1948
Report/Patent Number
NACA-TN-1517
Report Number: NACA-TN-1517
Accession Number
93R11491
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CONTROL SURFACES, SEALED-GAP
WIND TUNNEL TESTS - NACA (6'X4') WORK CARRIED ON AT LMAL
CONTROL SURFACES - HINGE MOMENTS EFFECT OF GAPS
CONTROL SURFACES - CHARACTERISTICS
AIRFOILS - NACA 009 - CHARACTERISTICS WING FLAPS

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