Investigation of Lateral Control Near the Stall Flight Tests with High-wing and Low-wing Monoplanes of Various Configurations
Fred E. Weick · H. Norman Abramson
Jan 1956 · National Advisory Committee for Aeronautics
Ebook
34
Pages
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About this ebook
Flight tests were made with one airplane having two different horizontal tail configurations in an attempt to provide an arrangement that would give near-optimum conditions with regard to the effect of power change on longitudinal trim near the stall. This attempt was successful with one d the configurations tested, so that under all of the conditions of power setting and center-of-gravity position tested the available elevator deflection was sufficient only to maintain the angle of attack at a point where lateral control remained adequate. The increase in minimum speed was negligible.
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