Metallic Thermal-Protection-System Panel Flutter Study

This work investigates thermal aeroelastic tailoring of a laminated composite panel with a lamination parameter-based method. Equivalent membrane and bending coefficients of thermal expansions for symmetric laminated panel are derived and represented with lamination parameters using Classical Laminated Plate Theory. The relationship between thermal flutter behavior and lamination parameters is examined. The optimization process is split into two stages. In the first stage, lamination parameters and laminate thicknesses are as design variables to minimize the structure mass, subject to thermal flutter behavior and feasible region constraints of lamination parameters. In the second-stage, instead of using conventional genetic algorithm, the enhanced JAYA method is extended to search the laminate configuration to target the optimal lamination parameters. The effectiveness of the presented method is demonstrated through a thermal aeroelastic tailoring problem.

show abstract

Microstructural evolution of ultrafine-grained NiCrCoAl foil after heat treatment at 1000°C

Zhang

Lin

et al. 2015

Materials Research Innovations

View full text Add to dashboard Cite

scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.

Contact Info

hi@scite.ai

10624 S. Eastern Ave., Ste. A-614

Henderson, NV 89052, USA

Blog Terms and Conditions API Terms Privacy Policy Contact Cookie Preferences Do Not Sell or Share My Personal Information

Made with 💙 for researchers

Part of the Research Solutions Family.

Metallic Thermal-Protection-System Panel Flutter Study

Cited by 10 publications

References 5 publications

Anisotropic phononic crystal structure with low-frequency bandgap and heat flux manipulation

Anisotropic phononic crystal structure with low-frequency bandgap and heat flux manipulation

Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA Algorithm

Microstructural evolution of ultrafine-grained NiCrCoAl foil after heat treatment at 1000°C

Contact Info

Product

Resources

About