Aerodynamic tests of an NACA 66(215)-116, a=0.6 airfoil with a 0.25.c slotted flap for the fleetwings XA-39 airplane
Wartime report ; L-629
1944
11 S., [15] Bl
graph. Darst
Originally issued November 1944 as Memorandum report L4K21
Report
English
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