The Limit of Stability of a Curved Plate Under Shear and Axial Stresses
Abstract
For an infinitely long plate of constant curvature, the buckling condition for combined shear and axial stresses was set up. The buckling condition was evaluated for the case of pure shear and an approximate formula was derived for the critical stresses for large curvatures. In connection with the discussion of the methods and results, the range of validity of the bucking condition set up is defined.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1939
- Accession Number
- ADA801471
Entities
People
- A. Kromm
Organizations
- National Advisory Committee for Aeronautics