Leading-edge buckling due to aerodynamic heating
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Leading-edge buckling due to aerodynamic heating
E. H. Mansfield
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3768
Date:
1959
Abstract:
A simple formula is derived for determining the onset of leading-edge buckling due to aerodynamic heating of wings which are either solid or thin-walled with a shear-resistant filling. The post-buckling behaviour is also investigated.
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Aeronautical Research Council Reports & Memoranda
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