Statistics: Effects of Horizontal-Tail Position and a Wing Leading-Edge Modification Consisting of a Full-Span Flap and a Partial-Span Chord-Extension on the Aerodynamic Characteristics in Pitch at High Subsonic Speeds of a Model With a 45 Degree Sweptback Wing

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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 60 times , with 4 in the last month . More information about this report can be viewed below.

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2019 2 3 4 3 12
2018 0 0 0 0 0 0 0 0 0 1 1 2 4
2016 0 0 0 0 0 1 0 0 0 1 0 0 2
2015 0 0 0 0 0 0 0 0 0 0 1 0 1
2014 3 0 2 1 0 11 4 1 3 0 0 0 25
2013 0 1 0 3 0 2 3 2 0 4 0 0 15
2012 0 0 0 0 0 0 1 0 0 0 0 0 1

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