A theoretical and experimental investigation of the effects of yaw on pressures, forces, and moments during seaplane landings and planing

Robert F. Smiley
naca-tn-2817
Nov 1952


A theory for the side force, rolling moment, yawing moment, and pressure distribution during yawed landings and planing of seaplanes was developed. For the special case of the straight-sided wedge without chine immersion, the results of the theoretical analysis are presented in the form of generalized curves covering all step landing conditions. Experimental impact and planing data are presented for a prismatic wedge having an angle of dead rise of 22.5 degrees and are shown to be in reasonable agreement with the theoretical predictions.

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