Aviation and Aeronautical Engineering

Aviation and Aeronautical Engineering

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B. Ford The results are summarized in the following table: _, , ... In this brief note, the wire and longeron stresses induced by the forces on the rudder are worked out for a single panel ... To allow for bending, it is suflicient to divide the rudder load equally between the upper and lower planes of the body, and to draw stress diagrams in these planes in the usual manner. ... X B (3 _ / FIG. 2 Thus in Fig. 3, where only those wires which are in tension in the longitudinal plane are shown, Iia#39; 1, , anbsp;...

Title:Aviation and Aeronautical Engineering
Publisher: - 1917


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