1. S. Metschan, Validated Feasibility Study of Integrally Stiffened Metallic Fuselage Panels for Reducing Manufacturing Costs. Cost Assessment of Manufacturing/design Concepts, NASA Contractor Report, NASA/CR-2000-209343, 2000.
2. J. Munroe, K. Wilkins, M. Gruber, Integral Airframe Structures (IAS) - Validated Feasibility Study of Integrally Stiffened Metallic Fuselage Panels for Reducing Manufacturing Costs, NASA Contractor Report, NASA/CR-2000-209337, 2000.
3. Non-prismatic sub-stiffening for stiffened panel plates – Stability behaviour and performance gains;Quinn;Thin-Walled Struct.,2010
4. A. Watson, C.A. Featherston, D. Kennedy, Optimization of post-buckled stiffened panels with multiple stiffener sizes, in: 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Honolulu, 2007. https://doi.org/10.2514/6.2007-2207.
5. M. Özakça, A. Murphy, S. van der Veen, Buckling and post-buckling of sub-stiffened or locally tailored aluminium panels, in: 25th International Congress of the Aeronautical Sciences, ICAS-2006, Hamburg, 2006. https://doi.org/10.13140/2.1.3074.2722.