1955•Unpublished venueRequires access
Experimental static aerodynamic forces and moments at low speed on a missile model during simulated launching from the 25-percent-semispan and wing-tip location of a 45 degree sweptback wing-fuselage combination
W. J. Alford, H Norman Silvers, Thomas J. King
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Abstract
Report presenting an investigation at low speed in the 300 mph tunnel to determine the static aerodynamic forces and moments on a missile model during simulated launching from 25-percent-semispan and wing-tip locations of a wing-fuselage combination. Results regarding the differences in location and effects induced by the fuselage are provided.