Investigation of Lateral Control Near the Stall: Flight Tests With High-Wing and Low-Wing Monoplanes of Various Configurations
Description: Report presenting the results of flight tests with several typical light aircraft. Flight tests were made with one airplane with two different horizontal tail configurations in an attempt to provide an arrangement that would give optimum conditions with regard to the effect of power change on longitudinal trim near the stall. The results are intended to provide quantitative flight-test information which may be useful to designers in attempting to provide for adequate low-speed control and which may be correlated with analytical analyses.
Date: June 1956
Creator: Weick, Fred E. & Abramson, H. Norman
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Partner: UNT Libraries Government Documents Department