Measurement of Flying Qualities of a Douglas A-26B Airplane (AAF No. 41-39120) 1: Longitudinal Stability and Control Characteristics
Description: Report discussing testing of the Douglas A-26B to determine the longitudinal stability and control characteristics. Information about the elevator, stick-fixed and stick-free stability, center of gravity, and flap effects are described.
Date: December 6, 1944
Creator: Crane, H. L.; Sjoberg, S. A. & Hoover, H. H.
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Partner: UNT Libraries Government Documents Department