1. Singer, J.; Rosen, A.: The Influence of Boundary Conditions on the Buckling of Stiffened Cylindrical Shells. TAE Report 213, Technion, Israel Institute of Technology, Dept. of Aeronautical Engineering, Haifa, Israel, June 1974.
2. van der Neut, A.: General Instability of Orthogonally Stiffened Cylindrical Shells. Collected Papers on Instability of Shell Structures —1962, NASA TN D-1510, pp. 309–319, Dec. 1962.
3. Singer, J.: Buckling of Integrally Stiffened Cylindrical Shells—A Review of Experiment and Theory. Contributions to the Theory of Aircraft Structures. Rotterdam: Delft University Press 1972, pp. 325–358.
4. Peterson, J. P.: Buckling of Stiffened Cylinders in Axial Compression and Bending-a Review of Test Data. NASA TN D-5561, December 1969.
5. Singer, J.; Arbocz, J.; Babcock, C. D.: Buckling of Imperfect Stiffened Cylindrical Shells Under Axial Compression. AIAA J. 9, No. 1, 68–75 (1971).