This is the second part of a three part report presenting the results of an investigation made to determine the feasibility of using wing installed aerodynamic devices for gust alleviation. This part presents the results of wind tunnel tests made to determine the aerodynamics effectiveness of several spoiler and flap configurations. The data obtained are presented in co-efficient form without analysis. Comparisons between the control effectiveness determined by these tests and the control effect¬iveness predicted by Part J of this report are shown in Part 1.
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