Download scientific diagram | Multi-stringer hat-stiffened panel from publication: Progressive Damage Analysis of a Multi-Stringer Post-Buckled Panel | Validation of a progressive damage finite element analysis model using the CompDam material model was performed on a large multi-stringer panel subjected to compressive loading. The panel had a Teflon insert embedded between the skin panel and stiffener to cause an ultimate | Damage, Joint Instability and Delamination | ResearchGate, the professional network for scientists.
Materials, Free Full-Text
Study of integral hat-stiffened composite structures manufactured
Frank LEONE, Research Aerospace Engineer
Materials, Free Full-Text
Frank LEONE, Research Aerospace Engineer, PhD (Mechanical Engineering & Mechanics), NASA, DC, Durability, Damage Tolerance, and Reliability Branch
Prediction method for shear stability of composite hat-stringer
Evaluation of a Metallic Repair on a Rod-Stiffened Composite Panel
PDF) Progressive Damage Analysis of a Multi-Stringer Post-Buckled
Design Optimization and Higher Order FEA of Hat-Stiffened
Full article: Numerical study of the influence of the stringers
Nelson DE CARVALHO, Engineer, PhD, NASA, DC, Durability, Damage Tolerance, and Reliability Branch