Statistics: Aerodynamic characteristics at a Mach Number of 6.8 of two hypersonic missile configurations, one with low-aspect-ratio cruciform fins and trailing-edge flaps and one with a flared afterbody and all-movable controls

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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 320 times , with 6 in the last month . More information about this report can be viewed below.

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2013 6 1 3 1 3 2 9 2 5 2 3 1 38
2012 0 2 2 2 0 0 3 3 0 0 0 2 14

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