1957•Unpublished venueRequires access
Effect of Fuselage Length and a Canopy on the Static Longitudinal and Lateral Stability Characteristics of 45 Degrees Sweptback Airplane Models Having Fuselages with Square Cross Sections
Byron M Jaquet, H. S. Fletcher
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Abstract
Report presenting a wind-tunnel investigation at low speed to determine the effects of fuselage nose length and a canopy on the static longitudinal and lateral stability characteristics of a complete model with a fuselage with square cross sections, a 45 degree sweptback wing, and a 45 degree sweptback horizontal tail.