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Effect of changing the mean camber of an airfoil sectionMethodical experiments with the series of airfoil sections of the same relative thickness and of variable relative cambers can be utilized for determining the effect of the camber on the aerodynamic properties of airfoil sections.
Document ID
19930085007
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Toussaint, A
Date Acquired
September 6, 2013
Publication Date
March 1, 1924
Report/Patent Number
NACA-TM-252
Accession Number
93R14297
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - S T AE 13A (S C 96-104) (ROYER) - CHARACTERISTICS
AIRFOILS - WIND TUNNEL TESTS
AIRFOILS - S T AE 25A-28A (S C 84-87) (DEWOITINE) - CHARACTERISTICS
AIRFOILS - MEAN CAMBER

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