NASA NACA-TR-1049-1951 Experimental investigation of the effect of vertical-tail size and length and of fuselage shape and length on the static lateral stability characteristics ofil s.pdf

1、REPORT 1049.EXPERIMENTAL INVESTIGATION OF THE EFFECT OF VERTICAL-TAIL SIZE AND LENGTHAND OF FUSELAGE SHAPE AND LENGTH ON THE STATIC IKrERAL STABILITYCHARACTERISTICS OF A MODEL WITH 45 SWEFTBACK WINGAND TAIL SURFACES 1 -By M. J. QUEIJO “and WALTEB D. iioLHAESUMMARYAn. investigation was made to determ

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