A study of the two-control operation of an airplane (1938)
NASA Technical Reports Server (NTRS) · leaf 6
e rolling -g<p moments. If the secondary moment is adverse and (28) exceeds a certain proportion of the rolling moment, an equilibrium condition in which the ailerons do not Thus the sideslip incident to turning with only rudder produce a bank of the airplane becomes possible. In control is mainly… … 1_ Lt_LT Figure L—Diagram Illustrating combined yawing and sideslipping motion during a (25) k W~NT steady two-control torn. Metacenterforyawlngmomentr,,—-jr1: metacenter for — Xi* * rolling momently— is obtained for the case of steady turning without side- slipping. This equilibrium is possible…
NASA Technical Reports Server (NTRS)
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