Static Analysis of Rigid Pavement Runway under the Influence of Aircraft Loading by Finite Element Technique

Autor: Sandeep Bharti, K Nallasivam, Khair Ul Wani

Publikováno v: Computational Engineering and Physical Modeling, Vol 5, Iss 4, Pp 79-101 (2022)

The runway is the most crucial part of any airport infrastructure and is designed to withstand the weight and impact of large aircraft. Runways must be durable enough to resist deformation, cracking, and wear caused by constant traffic. Therefore, a

Externí odkaz: https://doaj.org/article/b3a29b20003348c58ba8c23ff6571366

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

Identification of the key design inputs for the FEM-based preliminary sizing and mass estimation of a civil aircraft wing box structure

Autor: Chao You, Mehdi Yasaee, Shun He, Daqing Yang, Yigeng Xu, Iman Dayyani, Hessam Ghasemnejad, Shijun Guo, Phil Webb, James Jennings, Giovanni Federico

FEM-based preliminary structural sizing has been successfully carried out for a typical single-aisle wing box structure using MSC Nastran, by considering various load cases representing typical aircraft manoeuvres, engine loads, landing and ground ha

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::eb91b0694b1477af0f6f6c3c015375c3
https://dspace.lib.cranfield.ac.uk/handle/1826/17379

Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.

Aircraft Loads – A Wide Range of Disciplinary and Process-Related Issues in Simulation and Experiment

Autor: Klimmek, T., Bogenfeld, R., Breitbarth, E., Dillinger, J., Handojo, V., Kier, T., Kohlgrüber, D., Pusch, M., Raab, C., Wild, J.

The estimation of the loads is a key aspect of the extensive aircraft design process and also an important task during the life-time of an aircraft. DLRs joint efforts regarding the loads estimation and application, the latter also in view of structu

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6488fcb29592601a38f90750593b7f5b
https://elib.dlr.de/135992/