Quantifying the sensitivity of plate aspect ratio and edge boundary conditions on CFRP plate impact and post impact residual strength

Autor: Quinn, Damian, Murphy, Adrian, Harley, Cara, Robinson, Trevor T., Nolan, Declan

Publikováno v: In Thin-Walled Structures January 2022 170

Propulsion system structural response to variation in aircraft architecture

Autor: Colbert, Stephen, Quinn, Damian, Nolan, Declan, Gaskell, Jillian, Fox, Rob

Publikováno v: Colbert, S, Quinn, D, Nolan, D, Gaskell, J & Fox, R 2023, Propulsion system structural response to variation in aircraft architecture . in AIAA AVIATION 2023 Forum: Proceedings . AIAA AVIATION Forum: Proceedings, American Institute of Aeronautics and Astronautics Inc. (AIAA), AIAA Aviation and Aeronautics Forum and Exposition (2023 AIAA AVIATION Forum), San Diego, California, United States, 12/06/2023 . https://doi.org/10.2514/6.2023-3520

Meeting future commercial sustainable aviation goals will require aircraft architectural configurations and propulsion systems that deviate from those currently employed today. Developing or selecting an optimal propulsion system solution for integra

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______2607::6f9489a449e2c71fd60c0e397fdc8dfa
https://pure.qub.ac.uk/en/publications/290a35d0-b979-46a9-8621-aeea34ead9ec

Integrating Allowable Design Strains in Composites with Whole Life Value

Autor: Price, Mark, Murphy, Adrian, Butterfield, Joe, Falzon, Brian, Quinn, Damian

Publikováno v: In Procedia CIRP 2013 11:278-283

Understanding the Influence of Powerplant Component Connection Strategies on Aircraft Engine Structural Deformations

Autor: Martin, Carrie, Quinn, Damian, Murphy, Adrian, Robinson, Trevor, Thompson, Katrina, Kirkland, Frank, Cottney, Derek, Fox, Rob, Gaskell, Jillian, O'Doherty-Jennings, James

Publikováno v: Martin, C, Quinn, D, Murphy, A, Robinson, T, Thompson, K, Kirkland, F, Cottney, D, Fox, R, Gaskell, J, O'Doherty-Jennings, J & Martin, C 2021, ' Understanding the Influence of Powerplant Component Connection Strategies on Aircraft Engine Structural Deformations ', Journal of Aircraft . https://doi.org/10.2514/1.C036275

In conventional aircraft design engine loads are transferred directly from the engine core and fan case to the pylon via engine mounts. Literature is available on the modelling of individual powerplant components but limited work is available on the

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c81336ef7ef3e4f41db756d5608f6060
https://pure.qub.ac.uk/en/publications/c8bab113-6f32-419f-9f7a-1afadd5334d6

Conceptual design of future aircraft structures incorporating dynamic loading

Autor: Colbert, Stephen, Quinn, Damian, Nolan, Declan, Fox, Rob, O'Doherty-Jennings, James

Publikováno v: Colbert, S, Quinn, D, Nolan, D, Fox, R & O'Doherty-Jennings, J 2020, ' Conceptual design of future aircraft structures incorporating dynamic loading ', 7th Aircraft Structural Design Conference, Limerick, Ireland, 07/10/2020-09/10/2020 .

The aviation industry’s progression toward unconventional, highly-integrated aircraft configurations, which are likely to experience dissimilar loading to conventional Tube-And-Wing aircraft, challenges the capabilities of existing conceptual desig

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______2607::7fabb9d2ca570004d82f559c9f610db2
https://pure.qub.ac.uk/en/publications/cfecf832-74af-4ca0-931d-460cba9bbd64