A theoretical and experimental investigation of the effects of yaw on pressures, forces, and moments during seaplane landings and planing / Robert F. Smiley.
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 generaliz...
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Format: | Government Document Book |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1952.
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2817. |
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Call Number: |
Y 3.N 21/5:6/2817
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Y 3.N 21/5:6/2817 | Available Place a Hold |