Experimental investigation of flutter and divergence characteristics of the rocket-motor fin of the ASROC missile: COORD. No. N-AM-66
Description: Report presenting testing of scale models of rocket-motor fins of the ASROC missile for flutter and divergence in the supersonic flutter tunnel over a range of Mach numbers. Results regarding the flutter boundary, type of flutter encountered, and effects of flutter are provided.
Date: July 31, 1958
Creator: Levey, Gilbert M. & Hanson, Perry W.
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