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Investigation of Lateral Control Near the Stall Flight Tests with High-wing and Low-wing Monoplanes of Various Configurations

Fred E. WeickH. Norman Abramson

出版	National Advisory Committee for Aeronautics, 1956
URL	http://books.google.com.hk/books?id=MtFCAQAAIAAJ&hl=&source=gbs_api
EBook	FULL_PUBLIC_DOMAIN

註釋

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.