Investigation of an All-Movable Control Surface at a Mach Number of 6.86 for Possible Flutter
Description:
Memorandum presenting results of tests for possible flutter of a dynamically and elastically scaled model of a proposed all-movable horizontal tail surface for the North American X-15 airplane. Tests at Mach number 6.86 were made on the scaled model and on several other configurations with lower stiffnesses.
Date:
May 8, 1958
Creator:
Lauten, William T., Jr.; Levey, Gilbert M. & Armstrong, William O.
Item Type:
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Partner:
UNT Libraries Government Documents Department