Výsledky vyhledávání - "Austin Pennington"

FEA-BASED FAILURE ANALYSIS OF POST-BUCKLED COMPOSITE MULTI-HAT STIFFENED PANEL UNDER STATIC COMPRESSION

Autor: VIJAY K. GOYAL, AUSTIN PENNINGTON

Publikováno v: American Society for Composites 2022.

The aerospace industry uses composite multi-hat stiffened panels for skins because of their high strength-to-weight and stiffness-to-weight ratios. However, laminated composites with initial flaws are susceptible to delamination under buckling loads.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::9f42a33f29907eabeaaf0f9fdcec8c26
https://doi.org/10.12783/asc37/36425

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Damage Prediction of Post-Buckled Composite Single Hat-Stringer Panel Subject to Compression After Impact

Autor: Vijay Goyal, Austin Pennington, Jason Action

Publikováno v: AIAA SCITECH 2022 Forum.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::cbb267c22b78a52152ea861b47919940
https://doi.org/10.2514/6.2022-2394

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PROGRESSIVE DAMAGE FAILURE ANALYSIS OF POST-BUCKLED COMPOSITE SINGLE-STRINGER PANEL WITH TEFLON INSERTS

Autor: Vijay K. Goyal, Jason Action, Austin Pennington

Publikováno v: American Society for Composites 2021.

The high strength-to-weight and stiffness-to-weight ratio materials, such as laminated composites, are advantageous for modern aircraft. Laminated composites with initial flaws are susceptible to delamination under buckling loads. PDA tools help enha

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::08c96b3a715c8cfd3886fcf293759cab
https://doi.org/10.12783/asc36/35773

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