The damping in roll of rocket-powered test vehicles having rectangular wings with NACA 65-006 and symmetrical double-wedge airfoil sections of aspect ratio 4.5
Description: Report presenting a free-flight investigation of two rocket-powered model configurations to determine the damping in roll. The model had rectangular wings of 4.5 aspect ratio and were the same except for the airfoil sections.Results regarding rolling velocity and total-drag coefficient are provided.
Date: March 29, 1950
Creator: Dietz, Albert E. & Edmondson, James L.
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