Statistics: Aerodynamic tests of an NACA 66(215)-116, a=0.6 airfoil with a 0.25c slotted flap for the Fleetwings XA-39 airplane

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This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and one other and was provided by UNT Libraries Government Documents Department to Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 1684 times , with 6 in the last month . More information about this report can be viewed below.

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Year January February March April May June July August September October November December Total
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2017 31 12 4 16 8 7 3 7 24 12 13 7 144
2016 38 39 33 29 18 35 21 23 13 29 46 28 352
2015 31 27 39 37 31 26 27 31 32 51 56 45 433
2014 17 19 33 23 16 17 22 31 19 36 24 30 287
2013 13 9 10 18 70 26 23 38 39 39 26 20 331
2012 9 9 5 3 4 7 0 51 7 8 10 15 128
2011 0 0 0 0 0 0 0 0 0 0 1 4 5

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