1953•Unpublished venueRequires access
A transonic investigation by the free-fall method of an airplane configuration having 45 degrees sweptback wing and tail surfaces
Stanley Faber, J. M. Eggleston
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Abstract
Report presenting a free-fall investigation of airplanes in the transonic range using a configuration with 45 degree sweptback wing and tail surfaces. The lift, drag, and longitudinal static and dynamic stability and control characteristics were obtained at a range of operating lift coefficients and Mach numbers.