Aerodynamic tests of an NACA 66(215)-116, a=0.6 airfoil with a 0.25c slotted flap for the Fleetwings XA-39 airplane Page: 1 of 39
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NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS
1 2 DEC 1947
November 1944 as
Memorandum Report L4K21
AERODYNAMIC TESTS OF AN NACA 66(215)-116, a = 0.6
AIRFOIL WITH A 0.25c SLOTTED FLAP FOR THE
FLEETWINGS XA-39 AIRPLANE
By Jones F. Cahill
Langley Memorial Aeronautical Laboratory
Langley Field, Va.
N A C A LIBRARY
LANGLEY MEMORIAL AERONAUTICAL
Langley Field; V.
NACA WARTIME REPORTS are reprints of papers originally issued to provide rapid distribution of
advance research results to an authorized group requiring them for the war effort. They were pre-
viously held under a security status but are now unclassified. Some of these reports were not tech-
nically edited. All have been reproduced without change in order to expedite general distribution.
L - 629
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Cahill, Jones F. Aerodynamic tests of an NACA 66(215)-116, a=0.6 airfoil with a 0.25c slotted flap for the Fleetwings XA-39 airplane, report, November 1944; (digital.library.unt.edu/ark:/67531/metadc61411/m1/1/: accessed August 20, 2017), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.