Elastic Instability of a Swept Panel: Analysis of the Buckling Tendency of a Panel of the Top Skin of a Swept Wing
Aircraft Engineering and Aerospace Technology
Article publication date: 1 February 1952
THE introduction of swept wings for certain high speed aircraft has brought with it a variety of fresh structural problems. The aero‐dynamic requirements of a smooth wing surface means that the designer must have information on the buckling characteristics of the top skin. If the ribs are parallel to the direction of flight a typical panel of skin will be in the form of a parallelogram, supported on two sides by stringers and on the other two sides by ribs.
Mansfield, E.H. (1952), "Elastic Instability of a Swept Panel: Analysis of the Buckling Tendency of a Panel of the Top Skin of a Swept Wing", Aircraft Engineering and Aerospace Technology, Vol. 24 No. 2, pp. 48-49. https://doi.org/10.1108/eb032130
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