October 03, 2019 article Towards a coupled structural and economical design procedure of unstiffened isotropic shell structures Thin-Walled Structures DOI: 10.1016/j.tws.2019.106416 OpenAlex Authors 0 Author list not loaded yet. Cited by 6 stored of 8 Search Sort Most cited Newest Oldest Patent citations Title Any typearticle review book-chapter conference-paper preprint dissertation book dataset other Any fieldAgricultural and Biological Sciences Arts and Humanities Biochemistry, Genetics and Molecular Biology Business, Management and Accounting Chemical Engineering Chemistry Computer Science Decision Sciences Dentistry Earth and Planetary Sciences Economics, Econometrics and Finance Energy Engineering Environmental Science Health Professions Immunology and Microbiology Materials Science Mathematics Medicine Neuroscience Nursing Pharmacology, Toxicology and Pharmaceutics Physics and Astronomy Psychology Social Sciences Veterinary Open access Curved Shear Panel Theory as an Enabler for Gradient-Based Wing Optimization 2026 conference-paper Engineering Aeroelasticity and Vibration Control Open access 0 citations A Revised Shear Panel Formulation for Parallelogram Panels 2026 Aerospace article Engineering Aeroelasticity and Vibration Control Open access 0 citations Validity of the Shear Panel Theory as a Reduced Modelling Approach 2025 conference-paper Engineering Structural Load-Bearing Analysis Open access 2 citations Minimum stiffness criterion for ring frames of stringer frame stiffened shell structures 2022 Thin-Walled Structures article Engineering Structural Load-Bearing Analysis 6 citations Analysis of mass and cost drivers of unstiffened isotropic shell structures considering their imperfection sensitivity 2020 Thin-Walled Structures article Engineering Structural Load-Bearing Analysis 5 citations Panel buckling of stiffened shell structures with torsional stiff stringer 2020 Aerospace Science and Technology article Engineering Composite Structure Analysis and Optimization 16 citations 6 results References 0