Statistics: Rocket-Model Investigation to Determine the Lift and Pitching Effectiveness of Small Pulse Rockets Exhausted From the Fuselage Over the Surface of an Adjacent Wing at Mach Numbers From 0.9 to 1.8

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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 92 times , with 5 in the last month . More information about this report can be viewed below.

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2018 0 0 2 2 0 1 0 0 1 0 0 0 6
2017 2 1 0 0 2 1 0 2 1 4 0 1 14
2016 0 0 0 2 1 1 0 0 1 2 0 0 7
2015 2 1 0 0 1 1 0 3 0 2 3 0 13
2014 1 0 0 0 0 3 15 1 0 1 1 2 24
2013 2 0 0 0 0 0 2 9 0 1 0 1 15
2012 0 0 0 0 0 2 0 0 1 2 0 0 5

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