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Results of aerodynamic tests on slotted airfoils in the aerotechnical laboratory (S.T. Ae.) of Rhode St. Genese, BrusselsWe have investigated the maximum lift obtainable with slotted airfoils derived from a symmetrical airfoil. These should have a smaller profile drag than other slotted airfoils.
Document ID
19930090810
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Puvrez, Paul
Date Acquired
September 6, 2013
Publication Date
February 1, 1928
Report/Patent Number
NACA-TM-449
Report Number: NACA-TM-449
Accession Number
93R20100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - RHODE ST GENESE 40B - CHAR & MOMENTS WING SLOTS
AIRFOILS - RHODE ST GENESE 43C - CHAR & MOMENTS WING SLOTS
AIRFOILS - RHODE ST GENESE 40D - CHAR & MOMENTS WING SLOTS
AIRFOILS - RHODE ST GENESE 40A - CHAR & MOMENTS WING SLOTS
AIRFOILS - RHODE ST GENESE 40E - CHAR & MOMENTS WING SLOTS
AIRLOILS - RHODE ST GENESE 43A - CHAR & MOMENTS WING SLOTS
AIRFOILS - RHODE ST GENESE 40F - CHAR & MOMENTS WING SLOTS
AIRFOILS - RHODE ST GENESE 40C - CHAR & MOMENTS WING SLOTS
AIRFOILS - RHODE ST GENESE 40G - CHAR & MOMENTS WING SLOTS
AIRFOILS - RHODE ST GENESE 43B - CHAR & MOMENTS WING SLOTS

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