Download scientific diagram | 1: Reference geometry of the hat-stiffener. from publication: Exploration and validation of integrated lightweight structures with additive manufacturing and fiber-reinforced polymers | This thesis presents and explores a set of novel approaches for the development of hybrid, integrated, lightweight, structures by combining additive manufacturing (AM) with fiber-reinforced polymers (FRP) in layup processes. The presented methods combine the strengths of both | Principle-Based Ethics, Trusses and Tensile Test | ResearchGate, the professional network for scientists.
Delamination failure of composite top-hat stiffeners using finite element analysis - Raju, B Gangadhara Prusty, Don W Kelly, 2013
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Hat section: (a) without web stiffener (a ¼ 0, g ¼ 0) and (b) with web
Damage Prediction of Buckled Composite Single Stiffened Panel Subject to Static Compression
a) Schematic part diagram of hat stiffener (b) Cross section details
Aerospace, Free Full-Text
Top-hat crashboxes of thermoplastic fibre-metal-laminates processed in one-step thermoforming: Experimental and numerical study - ScienceDirect
Materials, Free Full-Text
1: Reference geometry of the hat-stiffener.
Design Optimization and Higher Order FEA of Hat-Stiffened Aerospace Composite Structures