An analysis of the forces and pressure distribution on a wing with the leading edge swept back 37.25 degrees
Description:
Report presenting testing of a semispan model of a wing with the leading edge swept back 37.25 degrees, an aspect ratio of 6.04, and a taper ratio of 0.5 in order to ascertain the compressibility effects on the forces, moments, and surface pressures. Lift, drag, and pitching-moment data along with chordwise distribution of static pressure at five spanwise stations are presented for a range of Mach numbers and a constant Reynolds number. Results regarding force and moment characteristics, critic…
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Date:
March 30, 1950
Creator:
Edwards, George G. & Boltz, Frederick W.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department