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Lift on a bent, flat plateThe lift on a bent, flat plate is calculated exactly by the use of conformal mapping. Results are presented in terms permitting direct determination of the angle of zero lift, the lift coefficient, and the lift-curve slope for any flap-chord ratio, flap-deflection angle, and angle of attack.
Document ID
19930093890
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Keune, Friedrich
Date Acquired
August 16, 2013
Publication Date
February 1, 1955
Report/Patent Number
NACA-TM-1340
Report Number: NACA-TM-1340
Accession Number
93R23215
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING FLAPS - DEFLECTION
CONFORMAL MAPPING FUNCTION
FINS & RUDDERS
LIFT - PLATES, FLAT
FLAPS, PLAIN - WING SECTIONS
WING FLAPS, HINGED
WING-SECTION THEORY
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